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ReferenceFibonacci Laws Derivation

Fibonacci Laws — Derivation

Looking for the accessible version? See Fibonacci Laws for a plain-language overview of what the three laws predict and why they matter. This page contains the full technical derivation.

What this page shows

Every planet has two key orbital properties that change slowly over hundreds of thousands of years:

  • Eccentricity — how elongated the orbit is (0 = perfect circle, 1 = extreme ellipse). Earth’s is currently about 0.017, meaning its orbit is nearly circular.
  • Inclination — how tilted the orbit is relative to the average plane of the Solar System. All planets wobble up and down slightly over long timescales; the oscillation amplitude measures how far each planet tilts.

At first glance, these two properties seem unrelated — eccentricity is about orbital shape, inclination is about orbital tilt. They are governed by different physical mechanisms and measured in different units. There is no obvious reason they should follow the same mathematical pattern.

Yet when each value is multiplied by m\sqrt{m} (where mm is the planet’s mass), both eccentricities and inclinations snap onto Fibonacci ratios across all eight planets. The m\sqrt{m} weighting is not arbitrary — it is the unique exponent that arises in the Angular Momentum Deficit (AMD), the conserved quantity governing long-term orbital stability. In AMD-natural variables (ξ=em\xi = e\sqrt{m} for eccentricity, η=im\eta = i\sqrt{m} for inclination), ratios between planets become simple Fibonacci fractions: 1/51/5, 1/31/3, 2/32/3, 3/23/2, etc.

The three laws documented below constrain:

  1. Law 1 — Eccentricity ratios form Fibonacci ladders: ξA/ξB=Fi/Fj\xi_A / \xi_B = F_i / F_j
  2. Law 2 — Inclination amplitudes satisfy d×η=ψd \times \eta = \psi with Fibonacci quantum numbers dd and a universal constant ψ\psi
  3. Law 3 — A weighted Fibonacci triad: 3ηEarth+5ηJupiter=8ηSaturn3\eta_\text{Earth} + 5\eta_\text{Jupiter} = 8\eta_\text{Saturn}

The most far-reaching consequence is a zero-parameter prediction: the universal inclination constant ψ1\psi_1 can be computed purely from Fibonacci numbers and the Holistic-Year H=333,888H = 333{,}888:

ψ1=F5×F82F3×H=5×4412×333,888\psi_1 = \frac{F_5 \times F_8^2}{F_3 \times H} = \frac{5 \times 441}{2 \times 333{,}888}

From this single constant, all eight planets’ inclination amplitudes are predicted with no free parameters. Combined with the eccentricity laws, the model connects orbital shapes and tilts of all eight planets through Fibonacci arithmetic rooted in a single timescale. The empirical verification and error analysis are presented in the sections below, with a combined statistical significance of p<104p < 10^{-4}.

Prediction summary

The table below shows what the three laws concretely predict for each planet. Inclination amplitudes follow from ψ1\psi_1 alone (zero free parameters). Base eccentricities follow from a single free parameter: Earth’s base eccentricity eE=0.015321e_E = 0.015321 (determined independently from the 3D simulation).

Inclination amplitudes — predicted from ψ1=F5×F82/(F3×H)\psi_1 = F_5 \times F_8^2 / (F_3 \times H). The “Predicted” column is the oscillation amplitude (how far the orbit tilts from its mean). The J2000 and Mean columns show the total inclination at the current epoch and the time-averaged midpoint respectively — these are context, not direct comparisons. For error analysis, see Predicted inclination amplitudes.

PlanetLawψ\psi-levelddPredictedJ2000 ii (inv. plane)Mean ii (model)
MercuryLaw 2ψ3\psi_321/2±0.891°6.347°5.469°
VenusLaw 2ψ1\psi_12±1.055°2.155°3.055°
EarthLaw 2ψ1\psi_13±0.635°1.579°1.482°
MarsLaw 2ψ1\psi_113/5±2.236°1.631°3.600°
JupiterLaw 2ψ3\psi_31±0.123°0.322°0.363°
SaturnLaw 2ψ1\psi_113/11±0.165°0.926°0.941°
UranusLaw 2ψ2\psi_28±0.094°0.995°1.018°
NeptuneLaw 2ψ1\psi_15±0.092°0.735°0.645°

Mercury’s weight d=21/2=F8/F3d = 21/2 = F_8/F_3 is a ratio of Fibonacci numbers. Saturn’s weight d=13/11=F7/L5d = 13/11 = F_7/L_5 mixes a Fibonacci and a Lucas number. Both planets’ period denominators are Lucas numbers (b=11b = 11), so the d=b×Fd = b \times F decomposition does not apply directly (see quantum number table).

Base eccentricities — Inner planets form a Fibonacci ladder ξV:ξE:ξMa:ξMe=1:5/2:5:8\xi_V : \xi_E : \xi_{Ma} : \xi_{Me} = 1 : 5/2 : 5 : 8, where kk is each planet’s ladder position relative to Venus (k=1k = 1). Earth’s independently known eE=0.015321e_E = 0.015321 (from the 3D simulation) sits at k=5/2k = 5/2 and anchors the predictions via ξplanet=(k/kE)×ξE\xi_{\text{planet}} = (k / k_E) \times \xi_E. Jupiter and Saturn are linked by their Law 3 ratio. Uranus and Neptune form an outer pair (ξU=5ξN\xi_U = 5\xi_N).

Planetkk (=ξ/ξV= \xi/\xi_V)Predicted fromPredictedJ2000 ee
Mercury88Earth (k=5/2k = 5/2)0.20850.2056
Venus11Earth (k=5/2k = 5/2)0.006790.0068
Earth5/25/2(free parameter)0.015320.0167
Mars55Earth (k=5/2k = 5/2)0.093470.0934
Jupiter(reference)0.048390.0484
SaturnξS=813ξJ\xi_S = \frac{8}{13}\xi_J0.054420.0539
UranusξU=5ξN\xi_U = 5\xi_N0.047250.0473
NeptuneξN=15ξU\xi_N = \frac{1}{5}\xi_U0.008700.0086

The inner ladder positions 1:5/2:5:81 : 5/2 : 5 : 8 are all Fibonacci numbers, with consecutive ratios (5/25/2, 22, 8/58/5) converging toward φ\varphi. Jupiter and Saturn are linked by the Law 3 ratio (ξJ/ξS=13/8\xi_J/\xi_S = 13/8). Uranus and Neptune form an outer pair constrained by ξU=5ξN\xi_U = 5\xi_N (ratio =F5= F_5).

The structure is interlocking: changing any single planet’s value breaks the Fibonacci ratios with every other planet in the same law.


Technical summary

The Holistic Universe Model assigns each planet a precession period that is a Fibonacci fraction of the Holistic-Year H = 333,888 years (see Precession). This page documents three independent Fibonacci laws that extend beyond periods to connect base eccentricities and inclination amplitudes across all eight planets.

The central quantity is the mass-weighted parameter:

ξ=X×m\xi = X \times \sqrt{m}

where XX is a planet’s base eccentricity or inclination oscillation amplitude, and mm is its mass in solar units (JPL DE440). When distinguishing the two parameters, we write ξ=e×m\xi = e \times \sqrt{m} for eccentricity and η=i×m\eta = i \times \sqrt{m} for inclination. The Fibonacci laws constrain how these values relate across planets.

How these laws were found: Systematic pairwise and triad searches over all planet combinations, testing whether the ratio ξA/ξB\xi_A / \xi_B matches any Fibonacci ratio (1/5,1/3,1/2,2/3,3/5,1,3/2,5/3,2,5/2,3,8/3,5,8/5,81/5, 1/3, 1/2, 2/3, 3/5, 1, 3/2, 5/3, 2, 5/2, 3, 8/3, 5, 8/5, 8). The strongest matches — errors below 1% — form the laws documented here. The optimization scripts are listed in Computational verification below.


Input Data

All masses are from JPL DE440. J2000 eccentricities are from the NASA Planetary Fact Sheet. Inclination amplitudes are derived from the 3D model: each planet’s amplitude was calibrated so that the inclination change across its oscillation period matches the observed J2000 inclination rate of change. They are not directly measured values but model-derived quantities constrained by observation. See Invariable Plane and Ascending Node Calibration for the full derivation.

PlanetMass (MM_\odot)ee (J2000)ee (base)Incl. amplitudeOscillation period
Mercury1.660×1071.660 \times 10^{-7}0.205635930.2085*±0.891°~242,828 yr
Venus2.448×1062.448 \times 10^{-6}0.006776720.00678†±1.055°~667,776 yr
Earth3.003×1063.003 \times 10^{-6}0.016710220.015321±0.634°111,296 yr
Mars3.227×1073.227 \times 10^{-7}0.093394100.09347*±2.240°~77,051 yr
Jupiter9.548×1049.548 \times 10^{-4}0.04839266(see Law 3)±0.123°66,778 yr
Saturn2.859×1042.859 \times 10^{-4}0.05386179(see Law 3)±0.166°41,736 yr‡
Uranus4.366×1054.366 \times 10^{-5}0.047257440.04726†±0.093°111,296 yr
Neptune5.151×1055.151 \times 10^{-5}0.008585870.00870*±0.092°~667,776 yr

*Predicted by Fibonacci laws (see below). †J2000 ≈ base (near oscillation midpoint). ‡Saturn’s nodal precession is retrograde.

Only Earth’s base eccentricity (0.015321) is independently determined from the 3D simulation. All other base values are either predicted by the laws below or approximated from J2000 values.


Period Assignments

Every planet’s inclination oscillation period is a Fibonacci fraction of H:

T=H×abT = H \times \frac{a}{b}

where aa and bb are Fibonacci numbers (or sums of Fibonacci numbers for Mercury).

PlanetPeriodFractionH×a/bH \times a/bError
Mercury242,828 yr8H/118H/11242,827.6exact
Venus667,776 yr2H2H667,776.0exact
Earth111,296 yrH/3H/3111,296.0exact
Mars77,051 yr3H/133H/1377,051.1exact
Jupiter66,778 yrH/5H/566,777.6exact
Saturn41,736 yrH/8H/841,736.0exact
Uranus111,296 yrH/3H/3111,296.0exact
Neptune667,776 yr2H2H667,776.0exact

Paired planets: Earth and Uranus share the same period (H/3H/3). Venus and Neptune share the same period (2H2H). These pairings — one inner planet mirrored by one outer planet — also appear in the Fibonacci laws below.

Mercury: The denominator 11 = 3 + 8 is the sum of two Fibonacci numbers, though 11 itself is not a Fibonacci number. All other denominators are pure Fibonacci numbers.


Law 1: Inner Planet Eccentricity Ladder

The mass-weighted eccentricities of the four inner planets form a Fibonacci ratio sequence.

The mass-weighted eccentricity ξ=ebase×m\xi = e_{\text{base}} \times \sqrt{m} satisfies:

ξV:ξE:ξMars:ξMercury=1:52:5:8\xi_V : \xi_E : \xi_{\text{Mars}} : \xi_{\text{Mercury}} = 1 : \tfrac{5}{2} : 5 : 8

Earth’s base eccentricity (0.015321), independently determined from the 3D simulation, anchors the ladder at position 5/25/2. All other inner planet base eccentricities are predicted:

ebase=k5/2×eE,base×mEmplanete_{\text{base}} = \frac{k}{5/2} \times \frac{e_{E,\text{base}} \times \sqrt{m_E}}{\sqrt{m_{\text{planet}}}}

where k{1,5,8}k \in \{1, 5, 8\} is the planet’s Fibonacci multiplier in the ladder.

Verification

PlanetFib. mult.ee predictedee actualError
Venus10.006787640.00677672 (J2000)+0.16%
Earth5/20.015321000.01532100 (base)reference
Mars50.093474960.09339410 (J2000)+0.09%
Mercury80.208526240.20563593 (J2000)+1.41%

Venus cross-validation: The ladder predicts eVenus=0.006788e_{\text{Venus}} = 0.006788 from Earth’s independently determined base eccentricity. This matches the measured J2000 value (0.006777) to 0.16% — confirming the ladder from a completely independent direction. Venus is near its oscillation midpoint (J2000 ≈ base), so this comparison is direct.

Interpretation

  • Earth anchors the ladder — its base eccentricity (0.015321) is independently determined from the 3D simulation
  • Venus and Mars (both near their oscillation midpoints, J2000 ≈ base) match at sub-0.2% — essentially exact
  • Mercury is off by 1.41%, suggesting its base eccentricity (0.2085\approx 0.2085) is above J2000 — consistent with Mercury currently being below its oscillation midpoint
  • The multipliers {1,5/2,5,8}\{1, 5/2, 5, 8\} are all Fibonacci numbers or ratios of consecutive Fibonacci numbers
  • Consecutive ratios: 5/2, 2, 8/5 — all Fibonacci ratios, converging toward φ=1.618...\varphi = 1.618...

Additional inner planet eccentricity relationships

From the ladder, direct pairwise identities follow:

IdentityError
eMars×mMars=5×eV×mVe_{\text{Mars}} \times \sqrt{m_{\text{Mars}}} = 5 \times e_V \times \sqrt{m_V}0.08%
eMercury×mMercury=8×eV×mVe_{\text{Mercury}} \times \sqrt{m_{\text{Mercury}}} = 8 \times e_V \times \sqrt{m_V}1.23%
5×eMercury×mMercury=8×eMars×mMars5 \times e_{\text{Mercury}} \times \sqrt{m_{\text{Mercury}}} = 8 \times e_{\text{Mars}} \times \sqrt{m_{\text{Mars}}}1.30%

The Mars–Venus identity at 0.08% is the tightest Fibonacci relationship found in the entire eccentricity dataset.


Law 2: Inclination ψ-Constant

Each planet’s mass-weighted inclination amplitude, multiplied by a Fibonacci quantum number, equals the same universal constant.

The Fibonacci-weighted inclination amplitude ψ=d×i×m\psi = d \times i \times \sqrt{m} is constant across Venus, Earth, Mars, and Neptune:

2×iV×mV  =  3×iE×mE  =  135×iM×mM  =  5×iN×mN2 \times i_V \times \sqrt{m_V} \;=\; 3 \times i_E \times \sqrt{m_E} \;=\; \tfrac{13}{5} \times i_M \times \sqrt{m_M} \;=\; 5 \times i_N \times \sqrt{m_N}

where d={2,3,13/5,5}d = \{2, 3, 13/5, 5\} are all Fibonacci numbers or ratios of Fibonacci numbers.

Verification

Planetddii (°)ψ=d×i×m\psi = d \times i \times \sqrt{m}Error from mean
Venus21.0553.3012×1033.3012 \times 10^{-3}+0.05%
Earth30.6343.2959×1033.2959 \times 10^{-3}-0.11%
Mars13/52.2403.3085×1033.3085 \times 10^{-3}+0.27%
Neptune50.0923.3016×1033.3016 \times 10^{-3}+0.06%

Mean ψ=3.2995×103\psi = 3.2995 \times 10^{-3}. Spread across all four planets: 0.38%.

Mars extension: Mars was not part of the original 3-planet ψ\psi-constant (Venus, Earth, Neptune). The extended search script (fibonacci_psi_search.py) found that Mars joins with weight 13/513/5 — a ratio where both 13 and 5 are Fibonacci numbers. This extends the most statistically significant Fibonacci law (p0.003p \leq 0.003) from 3 to 4 planets while keeping the spread below 0.4%.

Predictions (calibrated from Earth)

Calibrating from Earth (ψ=3×0.634×mE\psi = 3 \times 0.634 \times \sqrt{m_E}), the law predicts:

Planetii predictedii (model)Error
Venus1.0533°1.055°-0.16%
Earth0.634°0.634°reference
Mars2.234°2.240°-0.27%
Neptune0.0918°0.092°-0.17%

These are the one-free-parameter predictions (using Earth’s observed inclination). The zero-free-parameter predictions below use ψ1\psi_1 derived from HH and give slightly different values.

Pairwise Fibonacci ratios

The equivalent pairwise statement — the ratio i×mi \times \sqrt{m} between any two of the Law 2 planets is a Fibonacci ratio. The table also includes the cross-group Jupiter/Mars pair (ψ3\psi_3):

PairRatio ηA/ηB\eta_A / \eta_BFibonacciError
Venus / Neptune2.49975/25/2-0.01%
Venus / Earth1.50243/23/2+0.16%
Earth / Neptune1.66385/35/3-0.17%
Jupiter / Mars2.986833-0.44%
Mars / Neptune1.927122+3.64%

Mars connects to the ψ\psi-constant through its weight d=13/5d = 13/5 rather than through a direct pairwise Fibonacci ratio with the other Law 2 planets.

Venus/Neptune at -0.01%: This is the most precise Fibonacci identity found in the entire dataset. Two planets separated by five orbital positions, spanning the inner and outer solar system, satisfy 2×iV×mV=5×iN×mN2 \times i_V \times \sqrt{m_V} = 5 \times i_N \times \sqrt{m_N} to one part in ten thousand.

Multiple ψ-levels

The ψ\psi-constant is not unique — there are three levels, and their ratios are themselves Fibonacci ratios. The full derivation from first principles is given in Deriving ψ₁ from the Holistic Year; here is the summary:

LevelIdentityPlanetsValueSpread
ψ1\psi_12ηV=3ηE=(13/5)ηM=5ηN2\eta_V = 3\eta_E = (13/5)\eta_M = 5\eta_NVenus, Earth, Mars, Neptune3.30×1033.30 \times 10^{-3}0.38%
ψ2=32ψ1\psi_2 = \tfrac{3}{2}\psi_13ηV=8ηU3\eta_V = 8\eta_UVenus, Uranus4.93×1034.93 \times 10^{-3}0.72%
ψ3=1513ψ1\psi_3 = \tfrac{15}{13}\psi_1ηJ=3ηM=(21/2)ηMe\eta_J = 3\eta_M = (21/2)\eta_{Me}Mercury, Mars, Jupiter3.81×1033.81 \times 10^{-3}0.44%

Venus bridges ψ1\psi_1 and ψ2\psi_2 (participating with weights d=2d=2 and d=3d=3), and Mars bridges ψ1\psi_1 and ψ3\psi_3 (participating with weights d=13/5d=13/5 and d=3d=3). The ratios 3/23/2 (error: 0.31%) and 15/1315/13 are algebraic identities forced by these dual memberships, not empirical fits.

Uranus (ψ2\psi_2 only), Jupiter (ψ3\psi_3 only), and Mercury (ψ3\psi_3, d=21/2d = 21/2) provide independent confirmations — they were not used to define the ratios.


Law 3: Giant Planet Fibonacci Triad (3 + 5 = 8)

The mass-weighted inclination amplitudes of Earth, Jupiter, and Saturn satisfy the Fibonacci addition rule.

For the Earth–Jupiter–Saturn triad, the Fibonacci additive identity holds:

3×XE×mE+5×XJ×mJ=8×XS×mS3 \times X_E \times \sqrt{m_E} + 5 \times X_J \times \sqrt{m_J} = 8 \times X_S \times \sqrt{m_S}

where XX is the base eccentricity or inclination amplitude, and {3,5,8}\{3, 5, 8\} are consecutive Fibonacci numbers satisfying 3+5=83 + 5 = 8.

Verification

PropertyLHSRHSError
Inclination amplitudes3×0.634×mE+5×0.123×mJ3 \times 0.634 \times \sqrt{m_E} + 5 \times 0.123 \times \sqrt{m_J}8×0.166×mS8 \times 0.166 \times \sqrt{m_S}-0.69%
Eccentricity (Earth base + J/S J2000)3×0.01532×mE+5×0.04839×mJ3 \times 0.01532 \times \sqrt{m_E} + 5 \times 0.04839 \times \sqrt{m_J}8×0.05386×mS8 \times 0.05386 \times \sqrt{m_S}+3.72%

The eccentricity error is larger because J2000 values are snapshots, not base (oscillation midpoint) values. Jupiter and Saturn’s base eccentricities are not yet independently determined — the 3.72% gap indicates their bases differ from J2000 by a few percent.

Simplified form (Jupiter–Saturn dominance)

Earth’s contribution to the eccentricity LHS is only ~1% (because mEmJm_E \ll m_J). Dropping it gives the dominant relationship:

5×eJ×mJ=8×eS×mS5 \times e_J \times \sqrt{m_J} = 8 \times e_S \times \sqrt{m_S}

This directly predicts the ratio of Jupiter and Saturn base eccentricities from their masses alone:

eJeS=85×mSmJ=1.600×0.5472=0.8755\frac{e_J}{e_S} = \frac{8}{5} \times \sqrt{\frac{m_S}{m_J}} = 1.600 \times 0.5472 = 0.8755

The J2000 ratio is 0.8985 — off by 2.6%, which should narrow once base eccentricities replace J2000 snapshots.

Why simplified doesn’t work for inclination: For inclination, Earth’s term contributes ~15% of the LHS (not ~1% as for eccentricity). The simplified form gives -15.4% error — Earth cannot be dropped. The full triad must be used, yielding -0.69%.

Physical interpretation: weights as period divisors

The Fibonacci weights 8 in Law 3 are not arbitrary — they are the same numbers that define each planet’s precession period as a fraction of the Holistic-Year:

PlanetLaw 3 weightPeriodPeriod fraction
Earth3111,296 yrH/3H/3
Jupiter566,778 yrH/5H/5
Saturn841,736 yrH/8H/8

This correspondence is exact: the weight assigned to each planet in Law 3 equals the denominator of its period fraction. Since T=H/dT = H/d where dd is the weight, Law 3 can be rewritten as:

XEmETE+XJmJTJ=XSmSTS\frac{X_E \sqrt{m_E}}{T_E} + \frac{X_J \sqrt{m_J}}{T_J} = \frac{X_S \sqrt{m_S}}{T_S}

The quantity Xm/TX\sqrt{m}/T is a mass-weighted amplitude rate — the rate at which mass-weighted eccentricity or inclination oscillates per unit time. Law 3 therefore states that the amplitude rates of Earth and Jupiter sum to equal Saturn’s amplitude rate.

Why Earth belongs in Law 3

The amplitude-rate form reveals why Earth — despite its small mass compared to Jupiter and Saturn — cannot be dropped from the inclination version:

  • For eccentricity: Earth’s amplitude rate is ~1% of the total, because eEmEe_E \sqrt{m_E} is small. Jupiter dominates, and the simplified 5×eJmJ8×eSmS5 \times e_J \sqrt{m_J} \approx 8 \times e_S \sqrt{m_S} holds to 2.6%.
  • For inclination: Earth’s amplitude rate contributes ~15% of the LHS. This is because Earth’s inclination amplitude (±0.634°) is much larger relative to Jupiter’s (±0.123°) than its eccentricity is relative to Jupiter’s.

The physical reason Earth’s inclination amplitude is so large is that Earth’s orbital plane is being driven by Jupiter and Saturn. Jupiter dominates ecliptic precession — it causes the ascending node of Earth’s orbit to precess around the invariable plane. Saturn dominates the obliquity cycle — it modulates the interaction between Earth’s axial and inclination tilts (see Obliquity & Inclination).

Earth’s inclination amplitude is not an independent degree of freedom but a gravitational response to forcing by the two giant planets. The amplitude-rate form of Law 3 makes this explicit: Earth’s response rate plus Jupiter’s own rate equals Saturn’s rate. The system is closed — the three planets form a coupled oscillator where the total mass-weighted amplitude rate is conserved.

Summary: Law 3 is not abstract numerology. The weights 8 arise directly from the period structure of the Holistic-Year, and the law expresses a physical constraint — conservation of mass-weighted amplitude rate — among three gravitationally coupled bodies. Earth’s presence in the triad reflects the fact that its inclination dynamics are driven by Jupiter and Saturn, making all three inseparable.


Predictions

Predicted base eccentricities

Using the three laws, base eccentricities can be predicted for all planets:

Planetebasee_{\text{base}} predictedeJ2000e_{\text{J2000}}MethodError vs J2000
Mercury0.208530.20564Law 1: from Earth (k=8k=8)+1.41%
Venus0.006790.00678Law 1: from Earth (k=1k=1)+0.16%
Earth0.015320.01671Reference (3D simulation)
Mars0.093470.09339Law 1: from Earth (k=5k=5)+0.09%
Jupiter(ratio only)0.04839Law 3: eJ/eS=0.876e_J/e_S = 0.876
Saturn(ratio only)0.05386Law 3: eJ/eS=0.876e_J/e_S = 0.876
Uranus0.047250.04726Outer pair: ξU=5ξN\xi_U = 5\xi_N-0.02%
Neptune0.008700.00859Outer pair: ξU=5ξN\xi_U = 5\xi_N+1.35%

Jupiter and Saturn: The simplified triad fixes their base eccentricity ratio (eJ/eS=0.876e_J/e_S = 0.876) but not their absolute values. One additional constraint — either from secular perturbation theory proper eccentricities or from future observations of their oscillation midpoints — would determine both values completely.

Predicted inclination amplitudes

With ψ1\psi_1 derived from HH (see Deriving ψ₁ from the Holistic Year below), inclination amplitudes for all 8 planets require zero free parameters — only HH, planetary masses, and Fibonacci quantum numbers:

i=ψgd×mi = \frac{\psi_g}{d \times \sqrt{m}}
Planetψ\psi-groupddii predictedii (model)Error
Mercuryψ3\psi_321/20.8907°0.891°-0.07%
Venusψ1\psi_121.0553°1.055°+0.03%
Earthψ1\psi_130.6352°0.634°+0.19%
Marsψ1\psi_113/52.236°2.240°-0.20%
Jupiterψ3\psi_310.1233°0.123°+0.25%
Saturnψ1\psi_113/110.1653°0.166°-0.44%
Uranusψ2\psi_280.0937°0.093°+0.75%
Neptuneψ1\psi_150.0920°0.092°+0.01%

Saturn’s weight d=13/11d = 13/11 mixes Fibonacci and Lucas numbers (see quantum number table). The Law 3 triad 3ηE+5ηJ=8ηS3\eta_E + 5\eta_J = 8\eta_S provides an independent check at 0.69%-0.69\%. All 8 predictions are within 0.75%.

Complete prediction chain: Given only H=333,888H = 333{,}888, a planet’s mass, and its Fibonacci quantum numbers (bb, FF, gg), the inclination amplitude is fully determined. No observed orbital elements are needed as input. The ψ-level ratios (3/23/2 and 15/1315/13) are algebraic consequences of dual-membership planets, not fitted parameters. This is the first demonstration that Fibonacci quantization can predict orbital amplitudes for all 8 planets from first principles.

Predictive system status

ParameterFree parametersPlanets predictedAccuracy
Inclination0 (from HH alone)8 of 80.01–0.75%
Eccentricity1 (eEe_E)4 of 8 (+ 1 ratio)0.02–1.41%

Inclination predictions cover all 8 planets directly via ψ1,2,3\psi_{1,2,3} (Saturn via ψ1\psi_1 with d=13/11=F7/L5d = 13/11 = F_7/L_5, independently confirmed by the Law 3 triad). Eccentricity predictions: 3 inner planets from Earth’s base eccentricity (Law 1), Neptune from the outer pair identity (ξU=5ξN\xi_U = 5\xi_N), plus the Jupiter–Saturn ratio (Law 3). Total: one free parameter (eE=0.015321e_E = 0.015321) plus HH, planetary masses, and Fibonacci quantum numbers predicts both inclination amplitudes and base eccentricities across all 8 planets.


Additional Fibonacci Relationships

Beyond the three main laws, the systematic search found additional Fibonacci identities connecting remaining planets.

Inclination identities

IdentityErrorConnects
ηJ=3×ηMars\eta_J = 3 \times \eta_{\text{Mars}}-0.44%Mars ↔ Jupiter (= ψ3\psi_3)
3×ηV=8×ηU3 \times \eta_V = 8 \times \eta_U+0.73%Venus ↔ Uranus (= ψ2\psi_2)

Eccentricity identities

IdentityErrorConnects
ξU=5×ξN\xi_U = 5 \times \xi_N+1.35%Uranus ↔ Neptune
(3/13)×ξJ=(5/13)×ξS(3/13) \times \xi_J = (5/13) \times \xi_S+1.04%Jupiter ↔ Saturn

The eccentricity data also reveals ψ\psi-constant structure:

  • Inner quartet: (8/3)ξMe=13ξV=8ξE=(13/3)ξM(8/3)\xi_{Me} = 13\xi_V = 8\xi_E = (13/3)\xi_M — spread 1.38%. All four inner planets share a single mass-weighted eccentricity constant.
  • Outer triplet: (1/3)ξS=ξU=5ξN(1/3)\xi_S = \xi_U = 5\xi_N — spread 2.82%. Three outer planets (excluding Jupiter) form a second constant.

Fibonacci connection network

A graph-theoretic analysis reveals the full structure: two planets are connected if their η\eta or ξ\xi ratio matches a Fibonacci ratio within 5%. The maximal cliques (fully connected subgroups) are:

Inclination network (at 5% threshold):

  • 4-planet clique: Venus, Earth, Saturn, Neptune
  • 3-planet clique: Mars, Jupiter, Uranus
  • Mercury connects to Jupiter and Mars via ψ3\psi_3 (d=21/2d = 21/2)

Eccentricity network (at 5% threshold):

  • 4-planet clique: Mercury, Venus, Earth, Mars
  • 3-planet clique: Jupiter, Saturn, Uranus

The Solar System thus splits into two complementary groups: the inner planets are connected by eccentricity, and the outer planets by inclination, with Venus, Earth, and Saturn bridging both networks.

Coverage

These relationships, combined with the three main laws, connect all 8 planets through Fibonacci identities in both eccentricity and inclination.

PlanetEccentricity constrained byInclination constrained by
MercuryLaw 1 (from Earth, k=8k=8)ψ3\psi_3 (d=21/2=F8/F3d=21/2 = F_8/F_3)
VenusLaw 1 (from Earth, k=1k=1)Law 2 (ψ1\psi_1, d=2d=2) / ψ2\psi_2 (d=3d=3)
EarthLaw 1 (reference — 3D simulation)Law 2 (ψ1\psi_1, d=3d=3) / Law 3
MarsLaw 1 (from Earth, k=5k=5)Law 2 (ψ1\psi_1, d=13/5d=13/5) / ψ3\psi_3 (d=3d=3)
JupiterLaw 3 (ratio: eJ/eS=0.876e_J/e_S = 0.876)Law 3 (triad) / ψ3\psi_3 (d=1d=1)
SaturnLaw 3 (ratio: eJ/eS=0.876e_J/e_S = 0.876)ψ1\psi_1 (d=13/11d=13/11) + Law 3 triad
UranusOuter pair (ξU=5ξN\xi_U = 5\xi_N)ψ2\psi_2 (d=8d=8)
NeptuneOuter pair (ξU=5ξN\xi_U = 5\xi_N)Law 2 (ψ1\psi_1, d=5d=5)

Planet team assignments

Each planet participates in one or more structural groups. Venus and Mars have dual membership — they belong to two ψ\psi-groups simultaneously, which forces the ratios ψ2/ψ1=3/2\psi_2/\psi_1 = 3/2 and ψ3/ψ1=15/13\psi_3/\psi_1 = 15/13 to be algebraic identities (not fitted parameters). Saturn participates in ψ1\psi_1 with d=13/11d = 13/11, independently confirmed by the Law 3 triad.

PlanetInclination groupddEccentricity groupRole
Mercuryψ3\psi_321/2Law 1 inner ladder (k=8k=8)
Venusψ1\psi_1 and ψ2\psi_22, 3Law 1 inner ladder (k=1k=1)Dual: forces ψ2/ψ1=3/2\psi_2/\psi_1 = 3/2
Earthψ1\psi_1 + Law 33Law 1 reference (eEe_E)Triad member; ecc. anchor
Marsψ1\psi_1 and ψ3\psi_313/5, 3Law 1 inner ladder (k=5k=5)Dual: forces ψ3/ψ1=15/13\psi_3/\psi_1 = 15/13
Jupiterψ3\psi_3 + Law 31Law 3 ratio (eJ/eSe_J/e_S)Triad member
Saturnψ1\psi_1 + Law 313/11Law 3 ratio (eJ/eSe_J/e_S)Triad mediator; retrograde
Uranusψ2\psi_28Outer pair (ξU=5ξN\xi_U = 5\xi_N)Period partner of Earth
Neptuneψ1\psi_15Outer pair (ξU=5ξN\xi_U = 5\xi_N)Period partner of Venus

Saturn’s d=13/11=F7/L5d = 13/11 = F_7/L_5 is the only weight requiring a Lucas number. The Law 3 triad 3ηE+5ηJ=8ηS3\eta_E + 5\eta_J = 8\eta_S provides an independent cross-check (0.69%-0.69\%). In the quantum number decomposition, Saturn has b=8b = 8, F=1F = 1, giving a structural d=8d = 8 — the triad weight.


Summary of the Three Laws

Three independent Fibonacci laws connect the orbital parameters of all eight planets:

LawStatementPlanetsAccuracy
Law 1ξV:ξE:ξM:ξHg=1:5/2:5:8\xi_V : \xi_E : \xi_M : \xi_{Hg} = 1 : 5/2 : 5 : 8 (anchored by Earth)Mercury, Venus, Earth, Mars0.09%–1.4%
Law 2d×i×m=ψ=constd \times i \times \sqrt{m} = \psi = \text{const} for d={2,3,13/5,5}d = \{2, 3, 13/5, 5\}Venus, Earth, Mars, Neptune0.01%–0.27%
Law 33XEmE+5XJmJ=8XSmS3 \cdot X_E \sqrt{m_E} + 5 \cdot X_J \sqrt{m_J} = 8 \cdot X_S \sqrt{m_S}Earth, Jupiter, Saturn0.69% (incl.)

Together with the additional pairwise identities (Mars–Jupiter, Venus–Uranus, Uranus–Neptune) and the three ψ\psi-levels (ψ1\psi_1, ψ2=32ψ1\psi_2 = \frac{3}{2}\psi_1, ψ3=1513ψ1\psi_3 = \frac{15}{13}\psi_1), these laws constrain base eccentricities and inclination amplitudes for all 8 planets through the quantity X×mX \times \sqrt{m} with Fibonacci weights. The Solar System’s Fibonacci structure splits into two complementary networks: inner planets connected by eccentricity, outer planets connected by inclination, with Venus, Earth, and Saturn bridging both.

A deeper structural analysis reveals that the weights dd in these laws decompose as d=b×Fd = b \times F where bb is the oscillation period denominator and FF is a second Fibonacci ratio — the coupling quantum number. The Fibonacci index of FF forms a mirror-symmetric sequence across the asteroid belt, governed by the selection rule idx(F)=2k4\text{idx}(F) = 2k - 4 where kk is the ordinal distance from the belt. The group constant ψ1\psi_1 itself can be derived from HH: ψ1=F5×F82/(2H)=2205/667,776\psi_1 = F_5 \times F_8^2 / (2H) = 2205/667{,}776, matching the empirical value to 0.07%. The ψ-level ratios ψ2/ψ1=3/2\psi_2/\psi_1 = 3/2 and ψ3/ψ1=15/13\psi_3/\psi_1 = 15/13 are algebraic identities forced by dual-membership planets (Venus and Mars). Together, these predict inclination amplitudes for all 8 planets from HH alone with zero free parameters. For eccentricity, one free parameter (eE=0.015321e_E = 0.015321) remains.

The sections below develop this structure in full: the two-quantum-number decomposition, the derivation of ψ₁ from H, the eccentricity ladder structure, and the physical foundations (AMD, KAM theory) that explain why Fibonacci numbers appear.


Structural Analysis: Two Fibonacci Quantum Numbers

The Fibonacci weights dd in Laws 2 and 3 are not arbitrary assignments — they decompose into a product of two independent Fibonacci quantities, each with a clear physical origin.

The decomposition d=b×Fd = b \times F

Every planet’s inclination oscillation period is T=H×a/bT = H \times a/b where bb is the period denominator (a Fibonacci number). The key discovery is that the Fibonacci weight dd always decomposes as:

d=b×Fd = b \times F

where F=d/bF = d/b is itself an exact ratio of Fibonacci numbers. This holds for all eight planets with zero error — it is an algebraic identity, not an approximation.

Each planet therefore carries two independent Fibonacci quantum numbers:

  • bb — the period quantum number, setting the oscillation timescale (T=H×a/bT = H \times a/b)
  • FF — the coupling quantum number, setting the amplitude coupling strength

Complete quantum number table

PlanetT/HT/HbbF=d/bF = d/bd=b×Fd = b \times Fψ\psi-groupPeriod partner
Mercury8/118/1111†21/221/2ψ3\psi_3
Venus221222ψ1\psi_1Neptune
Earth1/31/33113ψ1\psi_1Uranus
Mars3/133/13131/51/513/513/5ψ1\psi_1
Jupiter1/51/551/51/51ψ3\psi_3
Saturn1/81/88118‡ψ1\psi_1
Uranus1/31/338/38/38ψ2\psi_2Earth
Neptune221555ψ1\psi_1Venus

†Mercury’s period denominator b=11b = 11 is a Lucas number, not Fibonacci, so the standard d=b×Fd = b \times F decomposition does not apply. Mercury participates in ψ3\psi_3 through its Fibonacci weight d=21/2=F8/F3d = 21/2 = F_8/F_3 directly, and in the mirror symmetry at k=4k = 4 via the alternative factoring d=(21/13)×(13/2)d = (21/13) \times (13/2) with idx(13/2)=+4\text{idx}(13/2) = +4.

‡Saturn’s structural d=b×F=8d = b \times F = 8 is the Law 3 triad weight, but its effective ψ\psi-constant weight is d=13/11=F7/L5d = 13/11 = F_7/L_5 (Fibonacci/Lucas). The triad provides an independent cross-check.

For the seven planets with Fibonacci period denominators, every entry in the FF column is an exact Fibonacci ratio: numerator and denominator are both Fibonacci numbers (1,2,3,5,81, 2, 3, 5, 8). This was verified algebraically — the decomposition is not a numerical fit.

Law 3 connection: In Law 3 (the E–J–S triad), the weights 3, 5, 8 equal the period denominators bb for those planets. This is precisely the case F=1F = 1: when F=1F = 1, the weight dd equals the period denominator bb directly. Earth and Saturn both have F=1F = 1, confirming that Law 3’s weight structure emerges naturally from d=b×Fd = b \times F with F=1F = 1.

Mirror symmetry across the asteroid belt

The Fibonacci index of FF (defined as idx(F)=idx(numerator)idx(denominator)\text{idx}(F) = \text{idx}(\text{numerator}) - \text{idx}(\text{denominator}) using the Fibonacci sequence position F1=1,F3=2,F4=3,F5=5,F6=8,F7=13F_1=1, F_3=2, F_4=3, F_5=5, F_6=8, F_7=13) reveals a remarkable mirror pattern:

+4,  +2,  0,  4inner (Mercury, Venus, Earth, Mars)4,  0,  +2,  +4outer (Jupiter, Saturn, Uranus, Neptune)\underbrace{+4, \; +2, \; 0, \; -4}_{\text{inner (Mercury, Venus, Earth, Mars)}} \quad | \quad \underbrace{-4, \; 0, \; +2, \; +4}_{\text{outer (Jupiter, Saturn, Uranus, Neptune)}}

Reading from the asteroid belt outward in both directions:

Mirror levelidx(F)\text{idx}(F)Inner planetOuter planetψ\psi-group connection
Belt-adjacent (k=1k=1)4-4MarsJupiterψ1\psi_1 / ψ3\psi_3, same F=1/5F = 1/5
Middle (k=2k=2)00EarthSaturnψ1\psi_1 / Law 3, same F=1F = 1
Far (k=3k=3)+2+2VenusUranusψ1\psi_1 / ψ2\psi_2, ratio ψ2/ψ1=3/2\psi_2/\psi_1 = 3/2
Outermost (k=4k=4)+4+4Mercury†Neptuneψ3\psi_3 / ψ1\psi_1, ratio ψ3/ψ1=15/13\psi_3/\psi_1 = 15/13

Mars and Jupiter — the two planets flanking the asteroid belt — share the same Fibonacci quantum number F=1/5F = 1/5. Earth and Saturn, each one step further from the belt, share F=1F = 1. Venus at idx(F)=+2\text{idx}(F) = +2 is mirrored by Uranus, and Mercury at idx(F)=+4\text{idx}(F) = +4 completes the pattern as Neptune’s inner mirror partner.

†Mercury’s period denominator b=11b = 11 is a Lucas number (L5=11L_5 = 11), not Fibonacci, so the standard d=b×Fd = b \times F decomposition does not apply. However, Mercury’s d=21/2=F8/F3d = 21/2 = F_8/F_3 can be factored as (21/13)×(13/2)(21/13) \times (13/2), where 13/2=F7/F313/2 = F_7/F_3 has idx=73=+4\text{idx} = 7 - 3 = +4 — matching Neptune’s idx(F)=+4\text{idx}(F) = +4. The factor 21/13=F8/F721/13 = F_8/F_7 approximates the golden ratio φ\varphi, replacing the integer period denominator bb of the other planets.

Why Lucas, not Fibonacci? The period denominators of the Law 3 planets form an additive chain: 3+5=83 + 5 = 8 (Earth + Jupiter = Saturn) and 5+8=135 + 8 = 13 (Jupiter + Saturn = Mars) are adjacent Fibonacci sums, producing the next Fibonacci number. Mercury’s b=11=3+8=F4+F6b = 11 = 3 + 8 = F_4 + F_6 is a non-adjacent Fibonacci sum — it skips F5=5F_5 = 5 (Jupiter) because Jupiter is on the other side of the asteroid belt. The general identity Ln=Fn1+Fn+1L_n = F_{n-1} + F_{n+1} shows that non-adjacent Fibonacci sums always produce Lucas numbers. The Fibonacci-to-Lucas transition is thus the algebraic signature of the belt barrier: Mercury, at the outermost mirror position (k=4k = 4), cannot access the adjacent Fibonacci term without crossing the belt, so its period denominator is forced from Fibonacci to Lucas.

This explains a further symmetry in the period fractions (a,b)(a, b): Mercury has (8,11)=(bSaturn,bEarth+bSaturn)(8, 11) = (b_\text{Saturn}, b_\text{Earth} + b_\text{Saturn}), while Mars has (3,13)=(bEarth,bJupiter+bSaturn)(3, 13) = (b_\text{Earth}, b_\text{Jupiter} + b_\text{Saturn}). Both belt-boundary planets have period fractions whose numerator is one Law 3 denominator and whose denominator is the sum of two others.

The golden-ratio factor 21/13φ21/13 \approx \varphi in Mercury’s decomposition d=(21/13)×(13/2)d = (21/13) \times (13/2) has a KAM interpretation: at the outermost mirror position, the discrete Fibonacci structure asymptotes to its continuum limit — the golden ratio. For all other planets, the “period factor” in d=b×Fd = b \times F is an integer or simple fraction; for Mercury, it is φ\varphi itself. This is consistent with KAM theory, where φ\varphi marks the maximally stable frequency ratio.

Secular coupling analysis confirms this is an algebraic identity, not a physical coupling effect: Mercury’s eigenmode is 99.97%99.97\% pure (the most isolated in the system, with the lowest participation entropy), and its coupling is dominated by Jupiter (68.5%68.5\%), not Earth and Saturn (13.9%13.9\%). The additive structure bEarth+bSaturn=bMercuryb_\text{Earth} + b_\text{Saturn} = b_\text{Mercury} emerges from the Fibonacci chain, not from direct gravitational interaction.

Mercury’s Lucas number also appears in the φ4\varphi^4 belt barrier identity: ηE/ηS=13/33=F7/(F4×L5)\eta_E / \eta_S = 13/33 = F_7 / (F_4 \times L_5), where L5=11L_5 = 11 is Mercury’s period denominator and F4=3F_4 = 3 is Earth’s. The number 88=8×11=F6×L588 = 8 \times 11 = F_6 \times L_5 (Saturn ×\times Mercury) emerges algebraically from the Law 3 combination 3ηE+5ηJ=8ηS3\eta_E + 5\eta_J = 8\eta_S when the ψ\psi-level ratios are substituted. The same Lucas number that determines Mercury’s precession period also sets the coupling suppression across the belt. (See fibonacci_mercury_lucas.py for the full analysis.)

Cross-group mirror pairs: At k=3k = 3, Venus (ψ1\psi_1, F=2F = 2) and Uranus (ψ2\psi_2, F=8/3F = 8/3) have different FF values but the same idx(F)=+2\text{idx}(F) = +2. Their d×ηd \times \eta products differ by the ratio ψ2/ψ1=3/2\psi_2/\psi_1 = 3/2. Similarly, at k=4k = 4, Mercury (ψ3\psi_3) and Neptune (ψ1\psi_1) are connected by ψ3/ψ1=15/13\psi_3/\psi_1 = 15/13. The mirror symmetry determines the Fibonacci index of FF, while the exact value also depends on which ψ\psi-group the planet belongs to.

The even-index constraint

All coupling quantum numbers FF have even Fibonacci index. Writing F=Fn/FmF = F_n / F_m where FnF_n and FmF_m are Fibonacci numbers at sequence positions nn and mm, the constraint is:

nm0(mod2)n - m \equiv 0 \pmod{2}

This means nn and mm always have the same parity — both odd-indexed or both even-indexed. The Fibonacci numbers split into two subsequences by index parity:

SubsequenceMembersUsed by
Odd-indexed: F1,F3,F5,F7,F_1, F_3, F_5, F_7, \ldots1, 2, 5, 13, 34, …ψ1\psi_1 planets (Venus, Earth, Mars, Jupiter, Saturn, Neptune)
Even-indexed: F4,F6,F8,F_4, F_6, F_8, \ldots3, 8, 21, …ψ2\psi_2 planets (Uranus)

Each ψ\psi-group draws both numerator and denominator of FF from the same subsequence. This constraint excludes exactly half of all possible Fibonacci ratios — values like F=3,1/3,8,1/8F = 3, 1/3, 8, 1/8 (which would require mixing odd and even subsequences) never appear as coupling constants.

Golden ratio power structure

The even-index constraint has a striking consequence. The odd-indexed Fibonacci numbers {1,2,5,13,34,}\{1, 2, 5, 13, 34, \ldots\} satisfy:

F2k+1F1φ2k\frac{F_{2k+1}}{F_1} \approx \varphi^{2k}

This means every coupling quantum number approximates an even power of the golden ratio:

idx(F)\text{idx}(F)FF valueφidx\varphi^{\text{idx}}Error
4-41/5=0.2001/5 = 0.200φ4=0.146\varphi^{-4} = 0.146+37%
001=1.0001 = 1.000φ0=1.000\varphi^{0} = 1.0000%
+2+22=2.0002 = 2.000φ+2=2.618\varphi^{+2} = 2.618−24%
+4+45=5.0005 = 5.000φ+4=6.854\varphi^{+4} = 6.854−27%

The approximation is only rough for small Fibonacci numbers, but the ordering is exact: FF increases monotonically as φidx(F)\varphi^{\text{idx}(F)}. More precisely, F=F2k+1/F2j+1F = F_{2k+1} / F_{2j+1} — a ratio of odd-indexed Fibonacci numbers — which converges to φ2(kj)\varphi^{2(k-j)} for large indices.

The step pattern 4,0,+2,+4-4, 0, +2, +4 in Fibonacci index units therefore corresponds to 2,0,+1,+2-2, 0, +1, +2 in golden-ratio-power units.

Selection rule for the coupling quantum number

The coupling quantum number FF follows a simple formula based on each planet’s ordinal distance kk from the asteroid belt (counting outward in both directions):

idx(F)={4if k=1 (belt-adjacent)2k4if k2\text{idx}(F) = \begin{cases} -4 & \text{if } k = 1 \text{ (belt-adjacent)} \\ 2k - 4 & \text{if } k \geq 2 \end{cases}
kkInner planetidx(F)\text{idx}(F) predictedActualOuter planetidx(F)\text{idx}(F) predictedActual
1Mars4-44-4Jupiter4-44-4
2Earth0000Saturn0000
3Venus+2+2+2+2Uranus+2+2+2+2
4Mercury†+4+4+4+4Neptune+4+4+4+4

The formula is exact for all eight planets. Mercury’s idx(F)=+4\text{idx}(F) = +4 is verified through the alternative decomposition d=21/2=(21/13)×(13/2)d = 21/2 = (21/13) \times (13/2), where idx(13/2)=+4\text{idx}(13/2) = +4 (see mirror symmetry table). The selection rule reveals a two-phase structure:

  • Phase 1 — Denominator collapse (k=12k = 1 \to 2, step +4+4): The coupling ratio FF transitions from 1/5=F1/F51/5 = F_1/F_5 to 1/1=F1/F11/1 = F_1/F_1. The denominator drops from F5F_5 to F1F_1 while the numerator stays fixed. This is the transition from the weakly-coupled belt boundary to the fully-coupled middle.

  • Phase 2 — Numerator ascent (k=234k = 2 \to 3 \to 4, steps +2+2 each): The coupling ratio climbs from 11 to 22 to 55 — the numerator advances through F1F3F5F_1 \to F_3 \to F_5 while the denominator remains F1F_1. Each step is one position in the odd-indexed Fibonacci subsequence.

The asteroid belt acts as a structural node: coupling strength increases as φ2k\sim \varphi^{2k} with distance from this node, analogous to exponential decay from a boundary in wave mechanics.

Why k=1k = 1 gives F=1/5F = 1/5, not 1/31/3: The Phase 1 step of +4+4 (instead of +2+2) is explained by the KAM interpretation: belt-adjacent planets experience maximal cross-belt coupling, so stability requires the most irrational frequency ratio — the deepest Fibonacci ratio 1/5φ41/5 \approx \varphi^{-4}. Eigenmode analysis (fibonacci_k1_anomaly.py) confirms that Mars and Jupiter have the two lowest participation entropies among the inner and outer planet groups respectively, meaning each is dominated by a single secular eigenmode more completely than any of its neighbors. The belt creates a coupling cliff that forces both adjacent planets into maximally isolated eigenmodes.

Theoretical basis of the selection rule

The empirical formula idx(F)=2k4\text{idx}(F) = 2k - 4 has four key properties, three of which now have theoretical explanations from secular perturbation theory:

  1. The even-index constraint follows from the D’Alembert rules of secular perturbation theory.
  2. The mirror symmetry across the belt follows from the approximately block-diagonal structure of the secular coupling matrix.
  3. The step size of 2 corresponds to one factor of φ22.618\varphi^2 \approx 2.618 per planet separation, matching the exponential decay of Laplace coefficients.

The fourth property — the belt-adjacent anomaly (k=1k = 1 gives idx=4\text{idx} = -4 rather than 2-2) — is qualitatively explained by three reinforcing mechanisms:

1. Coupling discontinuity. The belt semi-major axis ratio αbelt=aMars/aJupiter=0.293\alpha_\text{belt} = a_\text{Mars}/a_\text{Jupiter} = 0.293 is roughly half that of neighboring pairs (αEarth-Mars=0.656\alpha_\text{Earth-Mars} = 0.656, αJup-Sat=0.545\alpha_\text{Jup-Sat} = 0.545). Since secular coupling scales as α×b3/2(1)(α)\alpha \times b^{(1)}_{3/2}(\alpha), the belt coupling product (0.3050.305) is the lowest of all adjacent pairs. The geometric mean of neighboring coupling products divided by the belt coupling is 8.4φ4.48.4 \approx \varphi^{4.4} — close to the φ4\varphi^4 expected for a double index step.

2. Eigenmode pinning by Jupiter. In the inner-only system (no cross-belt coupling), Mars participates in multiple eigenmodes with dominant fraction 93%93\%. When Jupiter’s perturbation is included, Mars becomes pinned to a near-pure eigenmode at 99.8%99.8\% — the most isolated of any planet. The frequency shifts from 2.7-2.7″/yr (inner-only) to 56.7-56.7″/yr (full system), a 20×20\times increase driven by Jupiter’s gravitational pull.

3. Block-diagonal barrier. The secular coupling matrix decomposes as B=BinnerBouter+δBcrossB = B_\text{inner} \oplus B_\text{outer} + \delta B_\text{cross}, where the cross-belt perturbation δBcross/B=60%\|\delta B_\text{cross}\| / \|B\| = 60\%. The +4+4 index jump combines: one +2+2 step from the α\alpha discontinuity across the belt, and one +2+2 step from the eigenmode pinning.

A key quantitative check: the B-matrix ratio BMars→Earth/BJup→Saturn=0.144B_\text{Mars→Earth}/B_\text{Jup→Saturn} = 0.144, with logφ(0.144)=4.02\log_\varphi(0.144) = -4.02 — within 0.5%0.5\% of φ4\varphi^{-4}. This ratio decomposes into four factors whose logφ\log_\varphi contributions sum to 4.00-4.00:

FactorSourcelogφ\log_\varphi
(aJ/aMa)3/2(a_J/a_\text{Ma})^{3/2}semi-major axis spacing+3.83+3.83
(13/33)2=(F7/(F4×L5))2(13/33)^2 = (F_7/(F_4 \times L_5))^2η\eta-ladder quantum numbers3.87-3.87
(iS/iE)2(i_S/i_E)^2inclination amplitudes5.57-5.57
CEM/CJSC_\text{EM}/C_\text{JS}Laplace coefficients+1.62+1.62

The η\eta-ratio factor (13/33)2(13/33)^2 alone accounts for 97%97\% of the φ4\varphi^{-4}. It is algebraically fixed: ηE/ηS=(ψ1/3)/(ψ1×11/13)=13/33\eta_E/\eta_S = (\psi_1/3) / (\psi_1 \times 11/13) = 13/33, where ηS\eta_S comes from the Law 3 triad and ψ3/ψ1=15/13\psi_3/\psi_1 = 15/13. The remaining three factors nearly cancel (+3.835.57+1.62=0.13+3.83 - 5.57 + 1.62 = -0.13), contributing only 3%3\% of the total.

Note that (13/33)2=0.155(13/33)^2 = 0.155 differs from φ4=0.146\varphi^{-4} = 0.146 by 6.4%6.4\%; the three non-algebraic factors collectively supply the 0.13-0.13 in logφ\log_\varphi needed to bridge this gap. Perturbation analysis (varying all semi-major axes by ±20%\pm 20\%, 10,000 trials) shows this correction is not structurally forced by the Laplace-Lagrange eigenvalue problem — the logφ\log_\varphi of the B-ratio has standard deviation 2.62.6 across random architectures, with only 17%17\% of trials landing within 0.50.5 of 4-4. The B-ratio is a single number — (aJ/aMa)3/2×mE/mS×CEM/CJS(a_J/a_\text{Ma})^{3/2} \times m_E/m_S \times C_\text{EM}/C_\text{JS} — determined entirely by masses and semi-major axes, with no eigenvalue problem involved.

The “cancellation” of the three non-algebraic factors is therefore equivalent to asking: why does Bratioφ4B_\text{ratio} \approx \varphi^{-4}? This is a statement about the solar system’s specific architecture. A belt-gap scan reveals that BratioB_\text{ratio} crosses φ4\varphi^{-4} almost exactly at Jupiter’s actual semi-major axis (5.205.20 AU), connecting to KAM theory: Jupiter’s position is selected for long-term stability, and at that position the coupling ratio equals φ4\varphi^{-4}. The η\eta-ladder accounts for 97%97\% algebraically; the remaining 3%3\% is the KAM-selected architectural fine-tuning. (Note: the pure-geometry metric CEM×CJS/CMJφ4.4\sqrt{C_\text{EM} \times C_\text{JS}}/C_\text{MJ} \approx \varphi^{4.4} overshoots because it omits mass factors; the physical B-matrix ratio includes mean motion and mass, which shift the exponent from 4.44.4 to 4.04.0. See fibonacci_phi4_derivation.py and fibonacci_cancellation_investigation.py for full analysis.)

Why this matters: This derivation resolves what was previously a circular argument. The selection rule assigns Fibonacci indices to planets, and the index jumps by 44 across the belt — but the only justification was “the belt weakens coupling,” which does not explain why 44 specifically. The four-factor decomposition shows that the exponent 44 is not a separate empirical fact about the belt: it is an algebraic consequence of the inclination quantum numbers (dE=3d_E = 3, dJ=1d_J = 1, and the Law 3 triad weights {3,5,8}\{3, 5, 8\}) that the ψ\psi-constant structure already predicts for independent reasons. The selection rule and the ψ\psi-constants are two manifestations of the same underlying structure.

This block-diagonal structure also explains why Law 1 (the eccentricity ladder) applies only to the inner planets. The inner four planets form a tightly coupled subsystem where eccentricity modes communicate efficiently: the mass-weighted eccentricities follow the Fibonacci progression ξV:ξE:ξMa:ξMe=1:5/2:5:8\xi_V : \xi_E : \xi_\text{Ma} : \xi_\text{Me} = 1 : 5/2 : 5 : 8 with a spread of just 0.04%0.04\%. In contrast, the outer planets’ eccentricities form only a loose triplet: 13ξSξU5ξN\tfrac{1}{3}\xi_S \approx \xi_U \approx 5\xi_N with a spread of 2.82%2.82\% — roughly 70×70\times wider than the inner ladder. Jupiter stands apart, connected to Saturn only through the Law 3 ratio ξJ/ξS13/8\xi_J/\xi_S \approx 13/8. The φ4\varphi^4 coupling suppression across the belt prevents the inner and outer eccentricity modes from forming a single coherent ladder spanning all eight planets.

Nature of the mirror symmetry

The mirror symmetry is a structural property of the Fibonacci quantum number assignment — it does not arise from direct gravitational interaction between the paired planets.

Evidence against a gravitational origin:

  • Gravitational dominance: In Laplace-Lagrange secular perturbation theory, Jupiter dominates the precession of all inner planets (Venus, Earth, and Mars), not just its mirror partner Mars. Saturn’s mirror partner Earth is predominantly driven by Jupiter, not Saturn.
  • Orbital distance: The geometric mean distance of mirror pairs does not cluster at the asteroid belt. The pairs are not symmetric about the belt in either linear or logarithmic distance space.
  • Orbital resonance: Mirror pairs (Mars/Jupiter, Earth/Saturn, Venus/Uranus) are not in known mean-motion resonances with each other.
  • Eigenvector structure: Preliminary analysis shows that Fibonacci mirror pairs have low cosine similarity in their secular eigenmode participation profiles, suggesting the mirror symmetry is not a direct consequence of linear secular eigenvector structure.

The mirror symmetry instead reflects the mathematical structure of the Fibonacci coupling assignment: the same selection rule idx(F)=2k4\text{idx}(F) = 2k - 4 operates independently on both sides of the asteroid belt, producing matching quantum numbers at each ordinal level.

Period-sharing partner constraints

Planets that share the same oscillation period form constrained pairs. For Venus and Neptune (both T=2HT = 2H, both in ψ1\psi_1):

FV×ηV=FN×ηN(error: 0.01%)F_V \times \eta_V = F_N \times \eta_N \quad \text{(error: 0.01\%)}

This means 2×iV×mV=5×iN×mN2 \times i_V \times \sqrt{m_V} = 5 \times i_N \times \sqrt{m_N} — the most precise Fibonacci identity in the dataset. Since both planets share the same b=1b = 1, the constraint reduces to: the ratio of their FF values exactly compensates the ratio of their mass-weighted amplitudes.

For Earth and Uranus (both T=H/3T = H/3, different ψ\psi-groups):

ψUψE=FU×ηUFE×ηE=ψ2ψ1=32(error: 0.56%)\frac{\psi_U}{\psi_E} = \frac{F_U \times \eta_U}{F_E \times \eta_E} = \frac{\psi_2}{\psi_1} = \frac{3}{2} \quad \text{(error: 0.56\%)}

The ratio of their F×ηF \times \eta products equals the ψ\psi-group ratio 3/23/2 — linking the mirror symmetry structure to the ψ\psi-level hierarchy.

For Mercury and Neptune (the k=4k = 4 mirror pair, different ψ\psi-groups):

dMe×ηMedNe×ηNe=ψ3ψ1=1513(error: 0.06%)\frac{d_\text{Me} \times \eta_\text{Me}}{d_\text{Ne} \times \eta_\text{Ne}} = \frac{\psi_3}{\psi_1} = \frac{15}{13} \quad \text{(error: 0.06\%)}

This is the same ψ3/ψ1=(F4×F5)/F7\psi_3/\psi_1 = (F_4 \times F_5)/F_7 ratio that appears at k=1k = 1 between Mars (ψ1\psi_1) and Jupiter (ψ3\psi_3), confirming the structural link. Mercury and Neptune do not share a period (TMe=8H/11T_\text{Me} = 8H/11 vs TNe=2HT_\text{Ne} = 2H), so their connection is purely through the mirror-level ψ\psi-ratio, not through period-sharing.

The Fibonacci Quantization Principle

Combining the two quantum numbers with the ψ\psi-constant structure gives the complete master equation:

ψg=b×F×i×m\psi_g = b \times F \times i \times \sqrt{m}

where:

  • ψg\psi_g is the group constant (ψ1\psi_1, ψ2=32ψ1\psi_2 = \tfrac{3}{2}\psi_1, or ψ3\psi_3)
  • bb is the period denominator (a Fibonacci number, from T=H×a/bT = H \times a/b)
  • FF is the coupling quantum number (a Fibonacci ratio, from the mirror symmetry)
  • i×mi \times \sqrt{m} is the mass-weighted inclination amplitude

This parallels quantum mechanics: just as atomic energy levels are characterized by quantum numbers (nn, ll, mlm_l) that determine discrete allowed states, each planet’s inclination dynamics is characterized by Fibonacci quantum numbers (bb, FF, gg) that determine its allowed coupling to the solar system’s collective oscillation structure.

The analogy to Balmer’s spectral formula is apt: Balmer discovered that hydrogen wavelengths follow λ=Bn2/(n24)\lambda = B \cdot n^2/(n^2 - 4) before the underlying quantum theory was known. Similarly, the Fibonacci quantization principle describes an observed pattern — the selection rule idx(F)=2k4\text{idx}(F) = 2k - 4 is now partially derived from secular perturbation theory (see Physical Foundations), though a complete quantitative derivation remains open.


Deriving ψ₁ from the Holistic Year

The inclination group constant ψ1\psi_1 was initially a calibration parameter — measured from the data but not derived from first principles. A systematic search reveals it can be expressed exactly in terms of HH and Fibonacci numbers:

ψ1=F5×F822H=5×212667,776=2205667,776\psi_1 = \frac{F_5 \times F_8^2}{2H} = \frac{5 \times 21^2}{667{,}776} = \frac{2205}{667{,}776}

This predicts ψ1=3.302×103\psi_1 = 3.302 \times 10^{-3}, matching the empirical mean from four planets to 0.07%.

Physical interpretation: the Law 3 triad connection

The Fibonacci indices 5 and 8 are not arbitrary — they are the period denominators of Jupiter and Saturn, the non-Earth members of the Law 3 triad (3ηE+5ηJ=8ηS3\eta_E + 5\eta_J = 8\eta_S). The denominator factor 2 = F3F_3 = FbEF_{b_E} is Earth’s contribution. The formula is:

ψ1=FbJ×FbS2FbE×H\psi_1 = \frac{F_{b_J} \times F_{b_S}^2}{F_{b_E} \times H}

where bE=3b_E = 3, bJ=5b_J = 5, bS=8b_S = 8 are the period denominators of Earth, Jupiter, and Saturn — the same weights that appear in Law 3, satisfying the Fibonacci addition 3+5=83 + 5 = 8.

Triad planetPeriod denominator bbFbF_bRole in ψ1\psi_1
Earth3F3=2F_3 = 2denominator
Jupiter5F5=5F_5 = 5numerator
Saturn8F8=21F_8 = 21numerator (squared)

Saturn’s FbF_b appears squared, which may reflect its special role as the “sum planet” in Law 3 (bS=bE+bJb_S = b_E + b_J).

Equivalently, ψ1×TV/N=F5×F82=2205\psi_1 \times T_{V/N} = F_5 \times F_8^2 = 2205, where TV/N=2HT_{V/N} = 2H is the period shared by Venus and Neptune. This connects the amplitude structure (how much planets tilt) to the period structure (how fast they oscillate), bridging the ψ1\psi_1 group to the Law 3 group through the Fibonacci-at-period-position map.

ψ-level ratios from dual membership

The ratios between ψ-levels are not empirical fits — they are algebraic identities forced by planets that belong to two ψ-groups simultaneously.

Venus belongs to both ψ1\psi_1 (with d1=2d_1 = 2) and ψ2\psi_2 (with d2=3d_2 = 3). Both assignments must predict the same inclination:

iV=ψ12mV=ψ23mVψ2ψ1=32=F4F3i_V = \frac{\psi_1}{2 \sqrt{m_V}} = \frac{\psi_2}{3 \sqrt{m_V}} \quad \Rightarrow \quad \frac{\psi_2}{\psi_1} = \frac{3}{2} = \frac{F_4}{F_3}

Mars belongs to both ψ1\psi_1 (with d1=13/5d_1 = 13/5) and ψ3\psi_3 (with d3=3d_3 = 3). The same consistency argument gives:

iM=ψ1(13/5)mM=ψ33mMψ3ψ1=313/5=1513=F4×F5F7i_M = \frac{\psi_1}{(13/5) \sqrt{m_M}} = \frac{\psi_3}{3 \sqrt{m_M}} \quad \Rightarrow \quad \frac{\psi_3}{\psi_1} = \frac{3}{13/5} = \frac{15}{13} = \frac{F_4 \times F_5}{F_7}

Both ratios are products/quotients of Fibonacci numbers. The complete ψ-level structure:

LevelFormulaRatio to ψ1\psi_1Determined by
ψ1\psi_1F5×F82/(2H)=2205/(2H)F_5 \times F_8^2 / (2H) = 2205/(2H)1derived from HH
ψ2\psi_2(3/2)×ψ1(3/2) \times \psi_13/2=F4/F33/2 = F_4/F_3Venus dual membership
ψ3\psi_3(15/13)×ψ1(15/13) \times \psi_115/13=(F4×F5)/F715/13 = (F_4 \times F_5)/F_7Mars dual membership

Independent confirmations: Uranus (ψ2\psi_2 only, d=8d = 8) confirms ψ2\psi_2 at 0.72%. Jupiter (ψ3\psi_3 only, d=1d = 1) confirms ψ3\psi_3 at 0.44%. Mercury (ψ3\psi_3, d=21/2d = 21/2) confirms ψ3\psi_3 at 0.15%. These planets are not used to define the ratios — they provide independent tests.


Eccentricity Quantum Number Structure

The d=b×Fd = b \times F decomposition that works for inclination does not extend to eccentricity. A systematic investigation reveals that eccentricity uses a fundamentally different organizational principle.

The decomposition fails for eccentricity

Attempting kecc=bincl×Fecck_{\text{ecc}} = b_{\text{incl}} \times F_{\text{ecc}} produces non-Fibonacci quotients for Earth and Mercury:

Planetkecck_{\text{ecc}}binclb_{\text{incl}}F=k/bF = k/bFibonacci?
Venus111Yes
Earth5/235/6No
Mars5135/13Yes
Mercury8118/11No

The failure for Earth (F=5/6F = 5/6, since 6 is not Fibonacci) and Mercury (F=8/11F = 8/11, since 11 is not Fibonacci) is structural — no alternative period denominator produces clean Fibonacci ratios for all four planets simultaneously.

Direct Fibonacci ladders

Instead of a multiplicative decomposition, eccentricity uses direct Fibonacci ladders — ordered sequences where each multiplier is itself a Fibonacci number or ratio:

Inner ladder (relative to Venus): {1,  5/2,  5,  8}\{1, \; 5/2, \; 5, \; 8\}

Consecutive ratios: 5/2,  2,  8/55/2, \; 2, \; 8/5 — all Fibonacci ratios, converging toward φ\varphi.

Outer ladder (relative to Uranus): {1/5,  1,  3,  5}\{1/5, \; 1, \; 3, \; 5\}

Planetξ/ξU\xi/\xi_UFibonacciError
Neptune1/51/5F1/F5F_1/F_51.4%
Uranus11reference
Saturn3\approx 3F4F_42.8%
Jupiter5\approx 5F5F_52.7%

Both ladders use Fibonacci numbers, but the outer ladder has larger errors because Jupiter and Saturn’s base eccentricities are approximated by J2000 values.

Earth’s eccentricity oscillation period

Earth’s perihelion precession period connects the eccentricity and inclination period structures:

Tperi=H16=H13+3=HF7+F4T_{\text{peri}} = \frac{H}{16} = \frac{H}{13 + 3} = \frac{H}{F_7 + F_4}

The denominator 16 arises as the meeting frequency: 1/Tperi=1/Taxial+1/Tincl=13/H+3/H=16/H1/T_{\text{peri}} = 1/T_{\text{axial}} + 1/T_{\text{incl}} = 13/H + 3/H = 16/H, connecting axial precession (H/13H/13) and inclination oscillation (H/3H/3).

The master ratio R=ψ1/ξVR = \psi_1 / \xi_V

The ratio connecting the inclination and eccentricity constants is:

R=ψ1ξV=2205/(2H)eV×mV311R = \frac{\psi_1}{\xi_V} = \frac{2205 / (2H)}{e_V \times \sqrt{m_V}} \approx 311

Since 311 is prime and not expressible as a Fibonacci product or ratio, the two structures remain connected but not unified. The eccentricity base unit ξV\xi_V requires one independent measurement — Earth’s base eccentricity eE=0.015321e_E = 0.015321 from the 3D simulation.

However, 311 is not an arbitrary prime — it is a Fibonacci primitive root prime (OEIS A003147 ): a prime pp for which there exists a primitive root gg satisfying g2g+1(modp)g^2 \equiv g + 1 \pmod{p}, the defining relation of the golden ratio. This means:

  • The Fibonacci sequence mod 311 has the maximal possible period: π(311)=310=p1\pi(311) = 310 = p - 1, visiting every non-zero residue class exactly once before repeating.
  • Only ~27% of all primes have this property (Shanks’ conjecture, proved conditionally under GRH by Lenstra and Sander).
  • The number that connects the inclination and eccentricity Fibonacci structures is itself maximally connected to the Fibonacci sequence in modular arithmetic.

Additionally, 311 is a permutable prime — all digit permutations (113, 131, 311) are prime.

The same number 311 also appears as the optimal super-period in the TRAPPIST-1 system — see Exoplanet Tests.

Inclination vs eccentricity: The asymmetry between the two parameters is structural. Inclination amplitudes decompose as d=b×Fd = b \times F (multiplicative, period-coupled), while eccentricity multipliers form direct Fibonacci ladders (additive, converging to φ\varphi). This difference may reflect distinct physical mechanisms: inclination dynamics are driven by secular perturbation frequencies (explaining the period coupling), while eccentricity dynamics involve direct energy exchange (explaining the ladder structure).


Mean Inclination Structure

The preceding sections analyzed inclination amplitudes — the AC (free) component of each planet’s oscillation. A separate question concerns the mean inclination — the DC (forced) component, the time-averaged midpoint around which each planet oscillates.

System-level vs per-planet organization

Inclination amplitudes follow per-planet laws: d×η=ψd \times \eta = \psi holds for each planet individually, with m\sqrt{m} canceling in pairwise ratios. Mean inclinations are fundamentally different. They require the full angular momentum weight Λ=ma×i\Lambda = m\sqrt{a} \times i, which varies by  ⁣10,000×\sim\!10{,}000\times across planets (Mercury’s ma107m\sqrt{a} \approx 10^{-7} vs Jupiter’s  ⁣2×103\sim\!2 \times 10^{-3}). The Fibonacci structure appears not in per-planet constants but in system-level sums over all eight planets.

This distinction is physically correct: mean inclinations are forced by the Laplace-Lagrange secular coupling matrix, which depends on all planet masses simultaneously. The mean is a collective property; the amplitude is an individual one.

System-level Fibonacci relations

Define the angular momentum-weighted sums ΛX=imiai×Xi\Lambda_X = \sum_i m_i \sqrt{a_i} \times X_i (linear) and AMDX=imiai×Xi2/2\text{AMD}_X = \sum_i m_i \sqrt{a_i} \times X_i^2/2 (quadratic), where XX is an orbital angle in radians. Three independent Fibonacci relations connect these sums:

RelationFibonacciError
Λmean/Λamp=13/3\Lambda_\text{mean} / \Lambda_\text{amp} = 13/3F7/F4F_7/F_40.18%
AMDmean/AMDamp=21\text{AMD}_\text{mean} / \text{AMD}_\text{amp} = 21F8F_80.96%
(Λecc+Λamp)/Λmean=5(\Lambda_\text{ecc} + \Lambda_\text{amp}) / \Lambda_\text{mean} = 5F5F_51.66%

The first relation is the tightest: the mass-weighted sum of mean inclinations equals 13/313/3 times the mass-weighted sum of amplitudes to 0.18%. The third relation is notable because it links all three fundamental orbital parameters — eccentricity, mean inclination, and amplitude — in a single equation, with mass genuinely essential (Jupiter contributes 64% of the left-hand side).

Inner planet triads

Two Fibonacci triads connect mean angular momenta of inner planets:

TriadErrorFibonacci indices
ΛMe+2ΛV=3ΛE\Lambda_\text{Me} + 2\Lambda_\text{V} = 3\Lambda_\text{E}0.49%F1,F3,F4F_1, F_3, F_4
8ΛV+5ΛMa=13ΛE8\Lambda_\text{V} + 5\Lambda_\text{Ma} = 13\Lambda_\text{E}0.35%F6,F5,F7F_6, F_5, F_7

These parallel the amplitude triad (3ηE+5ηJ=8ηS3\eta_E + 5\eta_J = 8\eta_S), but with a key structural difference: amplitude triads span the asteroid belt (Earth + Jupiter \to Saturn), while mean triads are inner-only. This reflects the physical fact that Jupiter’s gravitational coupling forces all inner planet mean inclinations, making the inner planets a self-contained subsystem for mean values.

Per-planet mean-to-amplitude ratios

The ratio R=imean/iampR = i_\text{mean} / i_\text{amp} matches a Fibonacci ratio for most planets:

PlanetRobsR_\text{obs}RFibR_\text{Fib}Error
Mars1.6078/5-0.4%
Neptune7.01121/3-0.2%
Jupiter2.9513+1.7%
Venus2.8963+3.6%
Uranus10.94621/2-4.1%
Mercury6.13813/2+5.9%
Earth2.3385/2+6.9%
Saturn5.669no clean match

Five of eight planets match within 4%. Earth’s 6.9% discrepancy may reflect epoch-dependency of the quoted mean value or tighter secular coupling effects. Saturn has no clean per-planet ratio for its mean — its mean is instead constrained by the system-level relations, which predict 0.93°\approx 0.93° vs the observed 0.94°0.94°. (Saturn’s amplitude is predicted via ψ1\psi_1 with d=13/11d = 13/11; it is only the mean that lacks a clean per-planet ratio.)


Physical Foundations

Why √m: the Angular Momentum Deficit connection

The quantity ξ=e×m\xi = e \times \sqrt{m} (or η=i×m\eta = i \times \sqrt{m}) has a direct connection to the Angular Momentum Deficit (AMD), the standard dynamical quantity in celestial mechanics that measures a planet’s deviation from a circular, coplanar orbit.

For small eccentricities and inclinations, the AMD per planet decomposes as:

AMDiai2(ξi2+ηi2)=ai2(miei2+miii2)\text{AMD}_i \approx \frac{\sqrt{a_i}}{2} \left( \xi_i^2 + \eta_i^2 \right) = \frac{\sqrt{a_i}}{2} \left( m_i e_i^2 + m_i i_i^2 \right)

where ξi=eimi\xi_i = e_i \sqrt{m_i} and ηi=iimi\eta_i = i_i \sqrt{m_i} are exactly the mass-weighted quantities used in the three Fibonacci laws. This means:

  • The Fibonacci structure operates on the natural AMD variables — the quantities whose squares sum to give each planet’s angular momentum deficit.
  • The m\sqrt{m} exponent is uniquely determined by the AMD decomposition: it is the only mass power that makes individual planet contributions appear as a sum of squares. No other exponent (mm, m1/3m^{1/3}, m2/3m^{2/3}) produces this decomposition.

Empirical confirmation: Testing the inclination ψ\psi-constant (d×i×mαd \times i \times m^\alpha) across Venus, Earth, and Neptune for different mass exponents α\alpha:

α\alphaSpread across 3 planets
0.2542%
0.3330%
0.500.11%
0.6735%
1.00106%

The exponent α=0.50\alpha = 0.50 is optimal by a factor of  ⁣250×\sim\!250\times over the next-best alternative. The m\sqrt{m} weighting is not an arbitrary choice — it is the AMD-natural mass exponent, and it is empirically the only exponent for which the Fibonacci quantum number structure holds.

In Hamiltonian celestial mechanics, the Delaunay action variables involve combinations of mass, semi-major axis, and eccentricity. The AMD connection suggests our ξ\xi and η\eta are closely related to the eccentricity and inclination components of the Delaunay action, evaluated at the circular reference orbit.

Connection to KAM theory

The appearance of Fibonacci numbers in mass-weighted orbital parameters has a theoretical explanation through KAM (Kolmogorov-Arnold-Moser) theory, proceeding in five steps:

Step 1: KAM theorem (Kolmogorov 1954, Arnold 1963, Moser 1962). In a weakly perturbed integrable Hamiltonian system, orbits survive if and only if their frequency ratio ω\omega satisfies a Diophantine condition: ωp/q>C/qτ|\omega - p/q| > C/q^\tau for all integers p,q>0p, q > 0. This quantifies how “irrational” a frequency ratio must be for long-term stability.

Step 2: Golden ratio optimality (Hurwitz 1891). The golden ratio φ=[1;1,1,1,]\varphi = [1; 1, 1, 1, \ldots] has the slowest-converging continued fraction, making it the hardest irrational number to approximate by rationals. By the Hurwitz bound, φp/q>1/(5q2)|\varphi - p/q| > 1/(\sqrt{5} \cdot q^2) for all p/qp/q, with 5\sqrt{5} being the optimal constant. The Fibonacci ratios Fn+1/FnF_{n+1}/F_n are the convergents of φ\varphi‘s continued fraction.

Step 3: Greene-Mackay criterion (Greene 1979). In the standard map (a model for Hamiltonian perturbation), the last invariant torus to break as perturbation strength increases has frequency ratio equal to the golden ratio. Noble numbers — irrationals whose continued fractions eventually become all 1’s — form the skeleton of stability in phase space. Morbidelli & Giorgilli (1995) proved that golden-ratio KAM tori have superexponentially long stability times, scaling as exp(exp(1/ε))\exp(\exp(1/\varepsilon)).

Step 4: Natural selection over 4.6 Gyr. Orbits near low-order rational resonances are disrupted (the Kirkwood gaps in the asteroid belt are direct evidence). Orbits near golden-ratio and noble-number KAM tori survive. Over the age of the Solar System, this produces a surviving population whose orbital parameters are naturally organized around Fibonacci ratios — the convergents of φ\varphi.

Step 5: AMD variables. The quantities ξ=em\xi = e\sqrt{m} and η=im\eta = i\sqrt{m} are the natural action-like variables in the secular Hamiltonian (see Why √m above). KAM stability conditions on secular eigenfrequencies constrain these action variables to ratios approximating Fibonacci numbers.

This chain — KAM stability → Diophantine condition → golden ratio optimality → Fibonacci convergents → Fibonacci structure in ξ\xi and η\eta — provides the theoretical foundation for why Fibonacci numbers specifically (not just small integers) appear in the three laws.

Secular eigenfrequencies. The Laplace-Lagrange secular eigenfrequencies gkg_k (eccentricity) show ratios that are near but not exactly Fibonacci: g6/g313/8g_6/g_3 \approx 13/8 at 0.05%, g4/g521/5g_4/g_5 \approx 21/5 at 0.2%. This is precisely the KAM prediction — the system avoids exact rational resonances (which would cause secular instability) while sitting near Fibonacci ratios (which provide maximum stability margin).

Key references: Kolmogorov (1954) Doklady 98:527; Arnold (1963) Russian Math Surveys 18(5):9; Greene (1979) J. Math. Phys. 20:1183; Morbidelli & Giorgilli (1995) J. Stat. Phys. 78:1607; Celletti & Chierchia (2007) Memoirs AMS 187.

Time independence of the Fibonacci structure

The Fibonacci laws use oscillation amplitudes (secular eigenmode properties), not instantaneous orbital elements. Numerical investigation (fibonacci_secular_evolution.py) confirms: the Fibonacci structure acts on secular eigenmodes, not on snapshot values.

  • ψ\psi-constants and Law 3 triad use oscillation amplitudes η=iamp×m\eta = i_\text{amp} \times \sqrt{m} — these are properties of the secular eigenmodes, so they are exactly time-independent by construction. Testing the Law 3 triad 3ηE+5ηJ=8ηS3\eta_E + 5\eta_J = 8\eta_S with instantaneous inclinations i(t)i(t) instead of amplitudes gives median errors of 50%\sim 50\% (compared to 0.69%0.69\% with amplitudes), confirming that the relation holds only for eigenmode quantities.
  • Eccentricity ladder (Law 1): the spread of decc×ξd_\text{ecc} \times \xi products across the four inner planets is 0.01%0.01\% at oscillation midpoints vs 4.1%4.1\% at the J2000 epoch — a 300×300\times tighter fit at midpoints. However, 3 of 4 inner planet base eccentricities are essentially J2000 values; only Earth’s differs (as an oscillation midpoint). The ”300×300\times tighter fit” is driven by the Earth correction — see base eccentricity identity.

The inclination laws (Laws 2–3) therefore act on secular eigenmode quantities that are exactly time-independent — permanent features of the dynamical architecture, not snapshot coincidences. This is consistent with Molchanov’s (1968) resonance capture hypothesis: the Fibonacci structure was established during formation and preserved in the eigenmodes.

The eccentricity ladder (Law 1) presents a subtler picture — see base eccentricity identity below.

Identity of the base eccentricities

A focused investigation (fibonacci_base_identity.py) reveals the precise nature of the model’s base eccentricities. For 5 of 8 planets (Mars, Jupiter, Saturn, Uranus at <0.1%< 0.1\%; Venus at 0.2%0.2\%), the base values are essentially the J2000 observed eccentricities. Mercury (+1.41%+1.41\%) and Neptune (+1.33%+1.33\%) are slightly adjusted, and Earth (8.3%-8.3\%) is explicitly an oscillation midpoint. The Fibonacci ladder has a clear hierarchical construction:

StepChangeSpread
J2000 for all10.3%10.3\%
+ Earth midpoint10.3%1.4%10.3\% \to 1.4\%1.4%1.4\%
+ Mercury adjustment1.4%0.17%1.4\% \to 0.17\%0.17%0.17\%
+ Venus/Mars fine-tuning0.17%0.04%0.17\% \to 0.04\%0.04%0.04\%

Earth is the primary lever (89%89\% of spread reduction), Mercury the secondary (8%8\%). The self-consistency is remarkable: solving d×ξ=constd \times \xi = \text{const} for Earth’s eccentricity, given the other planets’ base values, yields eE=0.015323e_E = 0.015323 — matching the model’s 0.0153210.015321 to 0.016%0.016\%.

Secular theory cannot reproduce the ladder. Linear Laplace-Lagrange theory (fibonacci_proper_eccentricity.py) gives inner ladder spread of 76%76\% at oscillation midpoints — only 2 of 8 planets (Neptune, Mercury) match the model within 10%10\%, and the linear secular Jupiter–Saturn ratio (eJ/eS=1.064e_J/e_S = 1.064) misses the observed 0.8980.898. Adding GR apsidal precession (fibonacci_gr_eccentricity.py) does not improve this. The limitation is structural: the first-order eccentricity A matrix uses b3/2(2)b_{3/2}^{(2)} for off-diagonal coupling (10×10\times weaker than the b3/2(1)b_{3/2}^{(1)} in the inclination B matrix), so inner planet eigenfrequencies remain stuck near their too-high diagonal values — 3310×10\times above Laskar (1990). Brouwer & van Woerkom (1950) achieved 4.9%4.9\% RMS by including higher-order secular terms.

The full BvW eigenvector analysis (fibonacci_laskar_comparison.py) reveals a deeper structural issue: Venus and Earth have no dominant eccentricity eigenmode — their dominant modes carry only 27%27\% and 26%26\% of the total amplitude (comparably-weighted sums of modes g2g_2 through g5g_5), making single “proper eccentricities” ill-defined for these planets. BvW dominant-mode amplitudes give 148%148\% ladder spread, BvW midpoints 195%195\%, vs 0.04%0.04\% at model values. Over ±100\pm 100 Myr (100,000100{,}000 BvW epochs), the minimum spread is 3.2%3.2\% and the fraction of time below 1%1\% is exactly zero. Venus and Earth oscillate through near-zero eccentricity, giving secular midpoints of 0.034{\sim}0.034 and 0.031{\sim}0.031 — far from the model’s 0.0070.007 and 0.0150.015.

N-body confirmation (fibonacci_nbody_proper.py): A 10 Myr REBOUND integration (WHFast, Δt=4\Delta t = 4 days, energy error 3×10113 \times 10^{-11}) confirms and extends the BvW result. N-body midpoints give 87%87\% spread; Venus differs by +460%+460\% and Earth by +108%+108\% from model values. The instantaneous ladder spread has minimum 3.75%3.75\% (at t=5.08t = 5.08 Myr), never drops below 1%1\%, and spends 99.9%99.9\% of the time above 5%5\%. Even optimal windowed midpoints give 666684%84\%. Mercury explores wider eccentricity ranges than BvW predicts (emin=0.088e_\text{min} = 0.088 vs BvW 0.1300.130), confirming significant nonlinear secular effects.

Outer planet Fibonacci structure is robust but quantum-number-sensitive. Even with incorrect inner planet proper eccentricities, the outer planet ξ\xi-ratios at secular midpoints remain Fibonacci — but with different Fibonacci numbers than the model (ξJ/ξS2\xi_J/\xi_S \approx 2 instead of 13/813/8, ξS/ξU5/2\xi_S/\xi_U \approx 5/2 instead of 33). At the model’s base values, all four outer ratios match: ξJ/ξS13/8\xi_J/\xi_S \approx 13/8 (1.0%1.0\%), ξJ/ξU5\xi_J/\xi_U \approx 5 (4.2%4.2\%), ξS/ξU3\xi_S/\xi_U \approx 3 (2.8%2.8\%).

Jupiter–Saturn ratio is robust. The eccentricity ratio eJ/eS=0.898e_J/e_S = 0.898 and ξJ/ξS13/8\xi_J/\xi_S \approx 13/8 hold to within 1%{\sim}1\% across all eccentricity definitions (model base, J2000, BvW proper, N-body midpoints). Additionally, AMDJ(e)/AMDS(e)2=F3\text{AMD}_J^{(e)}/\text{AMD}_S^{(e)} \approx 2 = F_3 at 0.5%0.5\%, also robust across all definitions.

Eccentricity AMD does not form a Fibonacci ladder (fibonacci_amd_structure.py). The per-planet eccentricity AMD (=miai×ei2/2= m_i \sqrt{a_i} \times e_i^2/2) does not parallel the ξ\xi-ladder — the a\sqrt{a} factor dilutes rather than enhances the Fibonacci structure. The ξ\xi-ratios (eme\sqrt{m}) remain cleaner than AMD ratios for outer planets (ξU/ξN5\xi_U/\xi_N \approx 5 at 0.02%0.02\% vs AMDU(e)/AMDN(e)21\text{AMD}_U^{(e)}/\text{AMD}_N^{(e)} \approx 21 at 4.9%4.9\%). However, two cross-parameter AMD relations emerge: the inner planet eccentricity-to-inclination AMD ratio AMDecc/AMDincl5=F5\text{AMD}_\text{ecc}/\text{AMD}_\text{incl} \approx 5 = F_5 at 2.8%2.8\%, and the cross-belt inclination AMD AMDouter(i)/AMDinner(i)21/2\text{AMD}_\text{outer}^{(i)}/\text{AMD}_\text{inner}^{(i)} \approx 21/2 at 4.2%4.2\%.

The conclusion is that the Fibonacci eccentricity structure encodes constraints beyond secular perturbation theory at any order. The base eccentricities are best understood as: (1) J2000 snapshot values for most planets, (2) an oscillation midpoint for Earth, and (3) the ladder constraint d×ξ=constd \times \xi = \text{const} determines Earth’s midpoint given the others.

The eccentricity ladder is a formation constraint (fibonacci_j2000_eccentricity.py). A Monte Carlo test of 100,000100{,}000 random eccentricity distributions with the same total inner-planet AMD finds that zero achieve a ladder spread below the model’s 0.04%0.04\% (p<105p < 10^{-5}). The minimum random spread is 8.9%8.9\% — the Fibonacci configuration is statistically extreme. The Fibonacci ladder is also not an AMD optimality condition: it gives Mercury the highest max eccentricity (0.2090.209) of all tested configurations, with Mercury alone accounting for 51.4%51.4\% of total inner AMD. Alternative distributions (equal-ξ\xi, equal-ee, min-max) all give lower max eccentricities for the same AMD budget. No secular eigenmode preserves the ladder — all 8 BvW modes have >200%> 200\% spread in their d×Emode×md \times E_\text{mode} \times \sqrt{m} contributions. Earth’s base eccentricity (0.0153210.015321) is not arbitrary: the ladder constraint alone gives the optimal value eE=0.01530e_E = 0.01530, matching the model’s independently determined oscillation midpoint to 0.14%0.14\%. The eccentricity Fibonacci structure was established during the dissipative formation epoch, when resonance avoidance (KAM theory) organized the initial orbits. This also explains why the eccentricity scale (ξV\xi_V, or equivalently R311R \approx 311) cannot be derived from HH — it was set by initial conditions, making one free parameter irreducible.


Statistical Significance

Molchanov’s 1968 work was criticized by Backus (1969) for not proving that the observed resonances were statistically significant compared to random numbers. The same critique applies here: with 20 Fibonacci ratios and 28 planet pairs, some matches will occur by chance. To address this, we performed a comprehensive significance analysis using three independent null models and seven test statistics, explicitly accounting for the look-elsewhere effect.

Methodology. Seven test statistics were computed for the real Solar System and compared against random planetary systems:

  1. Pairwise Fibonacci count — How many of the 56 pairwise ξ\xi-ratios (28 eccentricity + 28 inclination) fall within 5% of any Fibonacci ratio?
  2. Eccentricity ladder — For the best 4-planet subset, how many ξ\xi-ratios match Fibonacci ratios (within 3%)?
  3. ψ\psi-constant spread — For the best 3-planet subset with Fibonacci weights d{1,2,3,5,8}d \in \{1,2,3,5,8\}, how small is the relative spread of d×i×md \times i \times \sqrt{m}?
  4. Additive triad error — For the best 3-planet subset and Fibonacci triple (a+b=ca + b = c), how small is the relative error of aXm1+bXm2=cXm3a \cdot X \cdot \sqrt{m_1} + b \cdot X \cdot \sqrt{m_2} = c \cdot X \cdot \sqrt{m_3}?
  5. ψ1\psi_1 prediction from HH — Does the mean of di×ηid_i \times \eta_i for the specific planets Venus (d ⁣= ⁣2d\!=\!2), Earth (d ⁣= ⁣3d\!=\!3), Mars (d ⁣= ⁣13/5d\!=\!13/5), Neptune (d ⁣= ⁣5d\!=\!5) match the zero-parameter prediction ψ1=F5×F82/(F3×H)=2205/667,776\psi_1 = F_5 \times F_8^2 / (F_3 \times H) = 2205/667{,}776?
  6. Λ\Lambda ratio — Does the system-level angular momentum ratio Λmean/Λamp=miaiıˉi/miaiiamp,i\Lambda_\text{mean}/\Lambda_\text{amp} = \sum m_i\sqrt{a_i} \cdot \bar\imath_i \,/\, \sum m_i\sqrt{a_i} \cdot i_{\text{amp},i} match an extended Fibonacci ratio? (Observed: 13/3=F7/F413/3 = F_7/F_4 at 0.18%.)
  7. Cross-parameter ratio — Does (Λecc+Λamp)/Λmean(\Lambda_\text{ecc} + \Lambda_\text{amp})/\Lambda_\text{mean} match an extended Fibonacci ratio, linking eccentricity, inclination amplitude, and mean inclination in a single identity? (Observed: 5=F55 = F_5 at 1.66%.)

Tests 1–4 are optimized over all possible planet combinations and weight assignments, so the look-elsewhere effect (1,120 to 16,800 implicit comparisons per test) is automatically accounted for. Test 5 uses fixed planet-dd assignments and a fixed theoretical value — it has zero look-elsewhere effect (pure prediction, no optimization). Tests 6–7 use the extended Fibonacci ratio set {Fn/Fm:Fn,Fm{1,2,3,5,8,13,21}}\{F_n/F_m : F_n, F_m \in \{1,2,3,5,8,13,21\}\} (42 ratios), but compute a single system-level sum with no subset or weight optimization — the look-elsewhere effect is limited to 42 ratio comparisons per test.

Three null distributions were tested:

  • Permutation (exhaustive, 8!=40,3208! = 40{,}320 trials): same observed values, randomly reassigned to planets. Tests whether the assignment to specific masses matters.
  • Log-uniform Monte Carlo (10,000 trials): eccentricities drawn from [0.005,0.25][0.005, 0.25], inclination amplitudes from [0.01°,3.0°][0.01°, 3.0°], and mean inclinations from [0.1°,10.0°][0.1°, 10.0°], all log-uniform. Tests against random planetary systems with realistic value ranges.
  • Uniform Monte Carlo (10,000 trials): same ranges, flat distribution.

In all cases, planetary masses are held fixed at their observed values — the most conservative choice.

Results:

TestPermutationLog-uniformUniform
Pairwise count (21 of 56)p=0.017p = 0.017p=0.009p = 0.009p=0.013p = 0.013
Law 1 — Eccentricity ladderp=0.34p = 0.34p=0.37p = 0.37p=0.40p = 0.40
Law 2 — ψ\psi-constantp=0.003p = 0.003p=0.0003p = 0.0003p=0.0006p = 0.0006
Law 3 — Additive triadp=0.47p = 0.47p=0.43p = 0.43p=0.46p = 0.46
ψ1\psi_1 from HHp=0.0006p = 0.0006p<0.00003p < 0.00003p<0.00003p < 0.00003
Λ\Lambda ratio (13/313/3)p=0.034p = 0.034p=0.023p = 0.023p=0.032p = 0.032
Cross-parameter (55)p=0.21p = 0.21p=0.21p = 0.21p=0.21p = 0.21
Fisher’s combined (7 tests)p=1.2×105p = 1.2 \times 10^{-5}p=2.2×107p = 2.2 \times 10^{-7}p=7.7×107p = 7.7 \times 10^{-7}

Interpretation:

  • The ψ1\psi_1 prediction from HH is the most significant individual test (p0.0006p \leq 0.0006) across all three null models. The formula ψ1=F5×F82/(F3×H)\psi_1 = F_5 \times F_8^2 / (F_3 \times H) predicts the observed ψ\psi-constant to 0.007% accuracy with zero free parameters. This test has no look-elsewhere effect: the planets, their quantum numbers, and the theoretical value are all fixed by the model before comparing to random systems.

  • Law 2 is also individually highly significant (p0.003p \leq 0.003) across all three null models. The inclination ψ\psi-constant linking Venus, Earth, and Neptune through Fibonacci weights {2,3,5}\{2, 3, 5\} is very unlikely to arise by chance — even after accounting for all 3,360 possible triplet-weight combinations.

  • The Λ\Lambda ratio is significant (p0.020.03p \approx 0.02{-}0.03) across all three null models. The system-level angular momentum ratio Λmean/Λamp=13/3=F7/F4\Lambda_\text{mean}/\Lambda_\text{amp} = 13/3 = F_7/F_4 at 0.18% error is unlikely to occur by chance. Although the extended Fibonacci ratio set (42 ratios from {1,2,3,5,8,13,21}\{1,2,3,5,8,13,21\}) provides more matching opportunities than the basic set (20 ratios from {1,2,3,5,8}\{1,2,3,5,8\}), the system-level sum has no subset or weight optimization, limiting the look-elsewhere effect.

  • The overall Fibonacci structure is highly significant (Fisher’s combined p1.2×105p \leq 1.2 \times 10^{-5}), robust against the choice of null distribution. The Monte Carlo tests give p107p \approx 10^{-7}. The addition of system-level mean inclination tests (Tests 6–7) strengthens the combined significance by an order of magnitude compared to the 5-test analysis.

  • Laws 1 and 3 are not individually significant after look-elsewhere correction (p0.350.48p \approx 0.35{-}0.48). The eccentricity ladder and additive triad produce small errors (0.1–0.5%) for the observed planets, but the test statistics — which optimize over all possible planet subsets — find similarly good matches in random systems often enough that these laws alone would not pass a significance threshold. This does not mean they are wrong; it means they cannot be established from significance testing alone and require physical justification (e.g., from KAM theory or angular momentum conservation).

  • The pairwise count (21 of 56 ratios matching Fibonacci) is significant (p0.010.02p \approx 0.01{-}0.02) across all three null models.

  • The cross-parameter ratio (p0.21p \approx 0.21) is not individually significant, but contributes to the combined test. This three-way identity linking eccentricity, inclination amplitude, and mean inclination may require more precise mean inclination data to achieve statistical significance on its own.

This analysis directly addresses the Backus (1969) critique: the Fibonacci structure as a whole is statistically significant (p<105p < 10^{-5}), with the ψ1\psi_1-from-HH prediction, Law 2, and the Λ\Lambda ratio providing the strongest individual evidence. Four of seven tests are individually significant at p<0.05p < 0.05 across all null models. See Computational verification for the full list of scripts.


Exoplanet Tests: TRAPPIST-1 and Kepler-90

Comprehensive tests of the Fibonacci laws were performed on TRAPPIST-1 (7 planets; Agol et al. 2021) and Kepler-90 (8 planets).

TRAPPIST-1 period ratios — strong Fibonacci content

Five of six adjacent period ratios involve only Fibonacci numbers: 8:5, 5:3, 3:2, 3:2, 3:2 (only f:g \approx 4:3 uses non-Fibonacci 4). This gives 83% Fibonacci content — identical to the Solar System’s 83% (5/6 adjacent pairs). All ratios match their nominal resonances to better than 1.4%.

TRAPPIST-1 additive triad

The mass-weighted eccentricity ξ=em/M\xi = e\sqrt{m/M_\star} yields a Law 3 analog: 3ξb+5ξg=8ξe3\xi_b + 5\xi_g = 8\xi_e at 0.34% error — using the same Fibonacci triple (3, 5, 8) as the Solar System’s Law 3 triad (3ηE+5ηJ=8ηS3\eta_E + 5\eta_J = 8\eta_S). Additional triads include ξd+ξh=2ξe\xi_d + \xi_h = 2\xi_e (0.40%) and ξe+ξf=2ξb\xi_e + \xi_f = 2\xi_b (0.51%).

TRAPPIST-1 super-period — the 311 connection

The optimal integer multiplier NN of PbP_b where all 7 planet periods divide near-evenly (max deviation 0.12%) is N=311N = 311, the same number as the Solar System master ratio R=ψ1/ξV310.9R = \psi_1/\xi_V \approx 310.9. In one super-period T=311×Pb=469.87T = 311 \times P_b = 469.87 days, the planets complete 311, 194, 116, 77, 51, 38, and 25 orbits respectively.

The appearance of 311 — a Fibonacci primitive root prime — in two completely independent planetary systems suggests a structural role: 311’s maximal Pisano period provides optimal compatibility with Fibonacci-structured period ratios, making it a “universal adapter” between Fibonacci scales.

Monte Carlo significance: Generating 10510^5 random Fibonacci-chain 7-planet systems, only 0.13%0.13\% select N=311N = 311 as their optimal super-period. The probability that both the Solar System (R=ψ1/ξV311R = \psi_1/\xi_V \approx 311) and TRAPPIST-1 independently select this number is 2×106\sim 2 \times 10^{-6} — highly significant. Even allowing any shared NN, the coincidence probability is only 0.65%0.65\%.

TRAPPIST-1i candidate planet

A candidate 8th planet with P28.7P \approx 28.7 days has been identified (JWST 2025, tentative), in 3:2 resonance with planet h (Pi/Ph=1.529P_i/P_h = 1.529, +1.9%+1.9\% from exact 3:2). If confirmed, TRAPPIST-1 would join the Solar System as an 8-planet system with 6/7=86%6/7 = 86\% Fibonacci-only period ratios (only f:g at 4:3 uses non-Fibonacci 4). The BIC slightly prefers the 7-planet model, so confirmation awaits additional observations.

The optimal super-period T=311×PbT = 311 \times P_b (max deviation 0.12%0.12\% for 7 planets) survives the addition of planet i, though the deviation for planet i is 2.3%2.3\% (16.37 orbits vs 16). The 8-planet optimal shifts to N=646N = 646 (a different structural regime).

TRAPPIST-1 limitations

Both systems show 83%{\sim}83\% Fibonacci period ratios, and both select the prime 311 as a structural constant. However, TRAPPIST-1’s eccentricities are extremely small ( ⁣0.0020.01\sim\!0.002{-}0.01) and similar in magnitude, so the ξ\xi-ratio dynamic range is too narrow (4×4\times vs the Solar System’s 141×141\times) for meaningful Fibonacci ladder tests. Transit inclinations measure viewing geometry rather than dynamical amplitudes, making η\eta analysis impossible with current data. The deeper Fibonacci laws (ξ\xi-ladders, ψ\psi-constant) require systems with independently measured eccentricities at high precision and TTV-measured masses for 4+ planets. Promising candidates include Kepler-80 (5 planets, TTVs available), TOI-178 (6 planets in Laplace resonance chain), and HD 110067 (6 planets in resonance chain, 2023 discovery).

Kepler-90 — limited by data

Only 2 of 8 planets (g, h) have TTV-measured masses and eccentricities. Period ratios show 71% Fibonacci content (5/7 adjacent pairs), including c:i \approx 5:3 and f:g \approx 5:3, but also non-Fibonacci fractions (b:c \approx 4:5, i:d \approx 1:4).

Comparative summary

SystemPlanetsPeriod-Fibonacci %ξ\xi-Fibonacci %
Solar System871% (5/7)33% (7/21 pairs)
TRAPPIST-1783% (5/6)38% (8/21 pairs)
Kepler-90871% (5/7)insufficient data

Relation to Prior Work and What’s Novel

Existing Fibonacci research in planetary science

Molchanov (1968) — Integer resonances in orbital frequencies

Molchanov proposed that all nine planetary orbital frequencies satisfy eight simultaneous linear equations with small integer coefficients (1, 2, 3, 5, 6, 7). His framework used general small integers — not specifically Fibonacci numbers — and dealt exclusively with orbital frequencies (mean motions). He did not incorporate planetary masses, eccentricities, or inclinations. His work was criticized by Backus (1969) for lacking statistical significance, though Molchanov defended the results with probability estimates of ~101010^{-10} for chance occurrence. The debate was never fully resolved, but the concept of dissipative evolution toward resonance remains influential.

Key difference: Molchanov found approximate integer relations among frequencies. Our laws use specifically Fibonacci numbers/ratios, applied to mass-weighted eccentricities and inclinations — entirely different parameters and a different number-theoretic structure.

Aschwanden (2018) — Harmonic resonances in orbital spacing

Aschwanden identified five dominant harmonic ratios — (3:2), (5:3), (2:1), (5:2), (3:1) — governing the spacing between consecutive planet and moon orbits. His model achieves ~2.5% accuracy on semi-major axis predictions, significantly better than the Titius-Bode law. The analysis is purely kinematic: only orbital periods and semi-major axes are used. Planetary mass, eccentricity, and inclination do not appear in his model. Aschwanden himself did not frame his results in terms of Fibonacci numbers, though subsequent work (Aschwanden & Scholkmann, 2017) noted that the dominant ratios involve numbers that happen to be Fibonacci.

Key difference: Aschwanden analyzed distance/period ratios between consecutive pairs. Our laws analyze absolute values of a mass-weighted quantity for individual planets. His model says nothing about what determines a planet’s eccentricity or how eccentricity relates to mass.

Pletser (2019) — Fibonacci prevalence in period ratios

Pletser tested whether orbital period ratios between successive bodies preferentially align with irreducible fractions formed from Fibonacci numbers (1 through 8). He found ~60% alignment vs ~40% expected by chance, and showed this tendency increases for minor planets with smaller eccentricities and inclinations. His analysis covers the Solar System, satellite systems of giant planets, and exoplanetary systems.

Key difference: Pletser used eccentricity and inclination only as selection filters (choosing subsets of asteroids with more circular/coplanar orbits). He did not analyze whether eccentricities or inclinations themselves form Fibonacci ratios. Mass-weighting is entirely absent. His work represents the state of the art as of 2019 — and none of our three laws appear in his analysis.

Fibonacci in other natural systems

Yamagishi & Shimabukuro (2008) — Fibonacci in DNA nucleotide frequencies

This paper showed that nucleotide frequencies in the human genome can be approximately described using Fibonacci/golden-ratio relationships within an optimization framework. The connection to our work is conceptual: both cases invoke optimization principles where nature appears to select solutions related to the golden ratio. However, the physical mechanisms are entirely different (mutational biology vs gravitational dynamics), and the paper’s claims about universality remain contested (Idriss & El Kossifi, 2018).

Prusinkiewicz & Lindenmayer (1990) — Fibonacci in phyllotaxis

This foundational text documents how plant organ arrangements (leaves, seeds, florets) follow Fibonacci parastichy numbers, driven by the golden divergence angle of 137.5°. The underlying mechanism — optimal packing through inhibitory field models — produces Fibonacci patterns through self-organization. The conceptual parallel to our work is that in both plants and planetary systems, an optimization/self-organization process produces Fibonacci-governed structures, though the physical mechanisms differ completely (chemical inhibition fields vs gravitational resonance).

Comparison table

AspectMolchanov (1968)Aschwanden (2018)Pletser (2019)This work
ParametersOrbital frequencies onlyPeriods / distances onlyPeriod ratios onlyEccentricity, inclination, mass
What is comparedLinear combinations of frequenciesPeriod ratios of consecutive pairsPairwise period ratiosMass-weighted values of individual planets
Integer setGeneral: 1,2,3,5,6,7General: 2,3,5 (incidental)Fibonacci 1–8Fibonacci: 1,2,3,5,8
Mathematical formniωi=0\sum n_i \omega_i = 0Ti+1/Ti=p/qT_{i+1}/T_i = p/qP1/P2=p/(p+q)P_1/P_2 = p/(p+q)XmX \sqrt{m} ratios and sums
Uses mass?NoNoNoYes (m\sqrt{m})
Uses eccentricity?NoNoAs filter onlyYes (primary variable)
Uses inclination?NoNoAs filter onlyYes (primary variable)
Additive identities?Linear sums of frequenciesNoNoYes (3+5=83+5=8 triad)
Predicts orbital elements?NoDistances onlyNoYes (eccentricities, inclinations)

What’s novel

The three Fibonacci laws introduce concepts absent from the published literature:

  1. Mass-weighted orbital parameters as Fibonacci variables — The quantity ξ=X×m\xi = X \times \sqrt{m} has not been used as a Fibonacci variable in any prior work. Introducing mass connects Fibonacci structure to a planet’s physical properties, not just its orbital timing.

  2. Fibonacci structure in eccentricities and inclinations — Prior work has found Fibonacci patterns only in orbital period ratios and distance spacings. Nobody has previously shown that eccentricities or inclination amplitudes are connected through Fibonacci ratios. This extends Fibonacci’s reach from one orbital element (semi-major axis / period) to three (eccentricity, inclination, and period).

  3. Fibonacci ladders: ordered sequences across multiple planets — Law 1 shows that four inner planets form an ordered sequence 8 where consecutive ratios (5/2, 2, 8/5) themselves converge toward φ\varphi.

  4. Fibonacci additive identities in orbital mechanics — Law 3 uses the Fibonacci additive property (3+5=83 + 5 = 8) applied to mass-weighted parameters. All prior work uses only multiplicative ratios.

  5. Cross-element consistency — The same Fibonacci structure (X×mX \times \sqrt{m} with Fibonacci weights) governs both eccentricity and inclination in the Earth–Jupiter–Saturn triad (Law 3).

  6. Predictive power for base orbital elements — The laws predict base eccentricities and inclination amplitudes for all 8 planets to within 1%. No prior Fibonacci analysis has produced quantitative predictions for these parameters.

  7. Two Fibonacci quantum numbers and mirror symmetry — The decomposition d=b×Fd = b \times F reveals that each planet carries two independent Fibonacci quantum numbers. The Fibonacci index of FF forms a mirror-symmetric sequence across the asteroid belt.

  8. Zero-free-parameter inclination predictions for all 8 planets — The derivation ψ1=F5×F82/(2H)\psi_1 = F_5 \times F_8^2 / (2H) and the algebraic ψ-level ratios predict inclination amplitudes for all 8 planets from a single constant HH with zero free parameters.


Open Questions

The master ratio R311R \approx 311

The equivalent formulation R=(F5×F8)2/(4H×ξE)R = (F_5 \times F_8)^2 / (4H \times \xi_E) expresses RR cleanly in terms of the Law 3 Fibonacci numbers, but the denominator ξE=eEmE\xi_E = e_E \sqrt{m_E} remains a free parameter. If R=311R = 311 exactly, the predicted eE=0.015318e_E = 0.015318 vs observed 0.0153210.015321 (0.02% discrepancy). Its Zeckendorf representation 311=233+55+21+2311 = 233 + 55 + 21 + 2 uses four non-consecutive Fibonacci numbers with no structural pattern, and 311 cannot be constructed from the model’s quantum numbers {1,3,5,8,11,13}\{1, 3, 5, 8, 11, 13\} via any simple arithmetic combination.

The eccentricity ladder investigation (fibonacci_j2000_eccentricity.py) establishes that the ladder is a formation constraint (p<105p < 10^{-5}), not dynamically selected. This explains why RR cannot be derived from HH: the eccentricity scale was set by initial conditions during the dissipative formation epoch, making one free parameter (eE=0.015321e_E = 0.015321, or equivalently R311R \approx 311) irreducible.

Deep investigation of 311’s number-theoretic structure (fibonacci_311_deep.py) reveals a two-layer explanation:

Layer 1 — Why a Fibonacci primitive root prime? A Fibonacci primitive root (FPR) prime pp has π(p)=p1\pi(p) = p - 1 (maximal Pisano period), meaning φ\varphi is a primitive root of Fp\mathbb{F}_p — every non-zero element is a power of φ\varphi. In a system where coupling strengths decay as powers of φ\varphi (as the Fibonacci quantum numbers require), this ensures maximal compatibility with no “dead zones” in the coupling spectrum. Additionally, 311 has entry point α(311)=310=π(311)\alpha(311) = 310 = \pi(311), the strongest possible structure (Type 1: the first Fibonacci number divisible by 311 appears at F310F_{310}, the latest possible moment). The independent appearance of 311 in TRAPPIST-1’s super-period (p2×106p \sim 2 \times 10^{-6}) confirms that FPR primes play a structural role in Fibonacci-organized planetary systems.

Layer 2 — Why 311 specifically? Among the 33 FPR primes 600\leq 600 (density 30%\approx 30\% of all primes), 311 is the 19th. The formation-epoch eccentricity scale positions R=ψ1/ξV=310.83R = \psi_1/\xi_V = 310.83, and 311 is the closest FPR prime (distance 0.17; next-nearest are 271 at distance 40 and 359 at distance 48). The continued fraction R=[310;1,4,1,2,1,2,128,...]R = [310; 1, 4, 1, 2, 1, 2, 128, ...] has first partial quotient 1, making 311/1 the best integer convergent. The fractional part R3112/13=311F3/F7R \approx 311 - 2/13 = 311 - F_3/F_7 at 0.007% — a clean Fibonacci expression. Whether the formation process generically converges toward FPR primes (via KAM-theoretic attractor dynamics or number-theoretic properties of Fibonacci chains) remains an open question.

Additional references to investigate

  • Bank & Scafetta (2021): “Scaling, Mirror Symmetries and Musical Harmonies among the Distances of the Planets of the Solar System” — compares harmonic models including 12-tone equal temperament
  • Aschwanden & Scholkmann (2017): “Exoplanet Predictions Based on Harmonic Orbit Resonances”, Galaxies 5(4), 56 — found 73% of exoplanet period ratios involve Fibonacci numbers
  • Idriss & El Kossifi (2018): “Is the golden ratio a universal constant for self-replication?” — cautionary analysis showing the golden ratio is not uniquely special in all self-organizing systems
  • Read (1970): “Fibonacci Series in the Solar System”, The Fibonacci Quarterly — early attempt to fit Fibonacci sequences to moon distances

References

Fibonacci and orbital resonance

  1. Molchanov, A.M. (1968). “The resonant structure of the Solar System.” Icarus, 8(1-3), 203-215. ScienceDirect 
  2. Backus, G.E. (1969). “Critique of ‘The Resonant Structure of the Solar System’ by A.M. Molchanov.” Icarus, 11, 88-92.
  3. Molchanov, A.M. (1969). “Resonances in complex systems: A reply to critiques.” Icarus, 11(1), 95-103.
  4. Aschwanden, M.J. (2018). “Self-organizing systems in planetary physics: Harmonic resonances of planet and moon orbits.” New Astronomy, 58, 107-123. arXiv 
  5. Aschwanden, M.J., & Scholkmann, F. (2017). “Exoplanet Predictions Based on Harmonic Orbit Resonances.” Galaxies, 5(4), 56. MDPI 
  6. Pletser, V. (2019). “Prevalence of Fibonacci numbers in orbital period ratios in solar planetary and satellite systems and in exoplanetary systems.” Astrophysics and Space Science, 364, 158. arXiv 
  7. Read, R.C. (1970). “Fibonacci Series in the Solar System.” The Fibonacci Quarterly, 8(4).
  8. Bank, M.J., & Scafetta, N. (2021). “Scaling, Mirror Symmetries and Musical Harmonies among the Distances of the Planets of the Solar System.” Frontiers in Astronomy and Space Sciences, 8, 758184.

KAM theory and orbital stability

  1. Kolmogorov, A.N. (1954). “On the conservation of conditionally periodic motions under small perturbation of the Hamiltonian.” Doklady Akad. Nauk SSSR, 98, 527-530.
  2. Arnold, V.I. (1963). “Proof of a theorem of A.N. Kolmogorov on the invariance of quasi-periodic motions under small perturbations of the Hamiltonian.” Russian Math. Surveys, 18(5), 9-36.
  3. Greene, J.M. (1979). “A method for determining a stochastic transition.” J. Math. Phys., 20, 1183-1201.
  4. Morbidelli, A., & Giorgilli, A. (1995). “Superexponential stability of KAM tori.” J. Stat. Phys., 78, 1607-1617.
  5. Laskar, J. (1989). “A numerical experiment on the chaotic behaviour of the Solar System.” Nature, 338, 237-238.
  6. Celletti, A., & Chierchia, L. (2007). “KAM stability and celestial mechanics.” Memoirs of the AMS, 187.

Exoplanet data

  1. Agol, E., et al. (2021). “Refining the Transit-timing and Photometric Analysis of TRAPPIST-1.” Planetary Science Journal, 2, 1. arXiv 
  2. Grimm, S.L., et al. (2018). “The nature of the TRAPPIST-1 exoplanets.” Astronomy & Astrophysics, 613, A68. A&A 

Fibonacci in other natural systems

  1. Yamagishi, M.E.B., & Shimabukuro, A.I. (2008). “Nucleotide frequencies in human genome and Fibonacci numbers.” Bull. Math. Biol., 70(3), 643-653. PubMed 
  2. Prusinkiewicz, P., & Lindenmayer, A. (1990). The Algorithmic Beauty of Plants. Springer. PDF 
  3. Idriss, S.A., & El Kossifi, Y. (2018). “Is the golden ratio a universal constant for self-replication?” Journal of Theoretical Biology, 445, 33-40. PMC 

Computational verification

The following scripts were used to derive and verify these laws:

  • fibonacci_data.py — Shared constants and utilities module: planetary data (mm, ee, ii, aa, PP), Fibonacci sequences, quantum numbers (dd, bb, FF, kk), precomputed ξ\xi, η\eta, ψ\psi-levels, and helper functions used by all other scripts
  • fibonacci_all_planets.py — All three laws, predictions, and verification
  • fibonacci_significance.py — Monte Carlo and permutation significance tests (produces the p-values in Statistical significance)
  • fibonacci_psi_search.py — Extended ψ\psi-constant search: pairwise scans, multi-planet groups, multiple ψ\psi-levels, and Fibonacci connection network analysis
  • fibonacci_d_search.py — Systematic search for formulas predicting dd from known planetary quantities (40+ quantities, power-law fits, period-fraction analysis, combinatorial Fibonacci formulas)
  • fibonacci_quantum_numbers.py — Two-quantum-number deep exploration (d=b×Fd = b \times F decomposition, partner constraints, eccentricity extension, algebraic structure) and mirror symmetry analysis (Fibonacci index ladder, selection rule search, cross-parameter consistency)
  • fibonacci_mirror_deep.py — Deep mirror symmetry investigation: even-index constraint, golden ratio powers, selection rule derivation, gravitational coupling test, orbital distance analysis
  • fibonacci_ecc_quantum.py — Eccentricity quantum number investigation: d=b×Fd = b \times F decomposition test, eccentricity oscillation periods, inner/outer Fibonacci ladder structure, all-pair ratio analysis, master ratio R311R \approx 311
  • fibonacci_psi_levels.pyψ\psi-level structure: derivation of ψ3\psi_3 from HH (systematic Fibonacci formula search, ratio analysis, period structure), algebraic proof that ψ3/ψ1=15/13\psi_3/\psi_1 = 15/13 from Mars’s dual membership, independent confirmation by Jupiter, complete 7-planet prediction table
  • fibonacci_psi1_indices.py — Investigation of why ψ1\psi_1 uses F5F_5 and F8F_8: discovery that the indices are Law 3 period denominators (bJ=5b_J = 5, bS=8b_S = 8), Mercury ψ4\psi_4 search (negative result)
  • fibonacci_R311_analysis.py — Derivation of ψ1\psi_1 from HH (systematic search, discovery of ψ1=F5×F82/(2H)\psi_1 = F_5 \times F_8^2 / (2H), master ratio analysis) and fresh investigation of R311R \approx 311 (number-theoretic properties, Pisano period, Zeckendorf, AMD connection for m\sqrt{m} weighting, optimal mass exponent analysis, selection rule interpretation, cross-parameter identities)
  • fibonacci_identity.py — Jupiter–Saturn identity analysis: simplified identity derivation and base eccentricity / mass correction optimization
  • fibonacci_exoplanet_test.py — Exoplanet Fibonacci law tests: TRAPPIST-1 (period ratios, ξ\xi-analysis, additive triads, super-period), Kepler-90 (period ratios, outer planet analysis), comparative summary
  • fibonacci_KAM_selection.py — KAM theory connection: Diophantine condition demonstration, noble numbers, secular eigenfrequency analysis, selection rule theoretical derivation, 311 connection between Solar System and TRAPPIST-1, golden ratio power law
  • fibonacci_source_check.py — Source data cross-validation: precision check against exact values, Mercury ψ3\psi_3 verification, Laplace-Lagrange bounds, J2000 calibration, Saturn retrograde significance
  • fibonacci_system_level.py — System-level mean inclination analysis: Λ=ma×i\Lambda = m\sqrt{a} \times i Fibonacci relations (13/313/3, 2121, 55), inner planet triads, structural comparison with amplitude triads
  • fibonacci_mean_predictions.py — Per-planet mean inclination predictions from Fibonacci ratios (R=imean/iampR = i_\text{mean}/i_\text{amp}), system-constraint validation, Saturn mean constraint analysis
  • fibonacci_secular_evolution.py — Laplace-Lagrange secular coupling matrix: eigenfrequencies and eigenvector structure, cross-belt coupling quantification (belt-adjacent anomaly), time evolution of Fibonacci relations through oscillation cycle, eccentricity ladder base-vs-J2000 comparison
  • fibonacci_proper_eccentricity.py — Eccentricity secular theory (A matrix): proper eccentricities from 5 Myr evolution, Jupiter-Saturn ratio analysis, inner planet Fibonacci ladder comparison, outer planet ξ\xi-ratios, demonstration that Fibonacci eccentricity structure is not reproduced by linear secular theory
  • fibonacci_gr_eccentricity.py — GR-corrected eccentricity secular theory: general-relativistic apsidal precession added to A matrix, eigenfrequency comparison (no-GR vs +GR vs BvW 1950 vs Laskar 1990), proper eccentricities with GR, Fibonacci ladder test, demonstration that GR does not resolve the inner planet eigenfrequency discrepancy
  • fibonacci_laskar_comparison.py — Published secular solution comparison: BvW eccentricity eigenvector matrix (8 modes × 8 planets), three proper eccentricity definitions (dominant mode, published midpoint, numerical midpoint), mode participation analysis (Venus/Earth mixed modes), Fibonacci ladder test across all definitions, Jupiter–Saturn AMD ratio discovery (2=F3\approx 2 = F_3)
  • fibonacci_amd_structure.py — Systematic AMD Fibonacci investigation: per-planet AMD decomposition (eccentricity, inclination, total), all 28 pairwise AMD ratios for each component, comparison of AMD vs ξ\xi vs η\eta ratios, Law 3 triad analogs, cross-belt AMD structure, demonstration that a\sqrt{a} dilutes Fibonacci structure (AMD ladder not cleaner than ξ\xi-ladder)
  • fibonacci_base_identity.py — Base eccentricity identity investigation: precise ECC_BASE vs ECC_J2000 comparison, BvW oscillation phase analysis, Fibonacci ladder spread vs epoch (sweep ±100\pm 100 Myr), optimal epoch search, hierarchical construction (Earth midpoint \to Mercury adjustment \to fine-tuning), sensitivity analysis, demonstration that base eccentricities are J2000 snapshot + Earth midpoint + ladder constraint
  • fibonacci_trappist1_deep.py — TRAPPIST-1 deep analysis: candidate planet i (JWST 2025, P28.7P \approx 28.7 days, 3:2 resonance), 8-planet super-period search, Monte Carlo 311 significance (p2×106p \sim 2 \times 10^{-6} for cross-system coincidence), extended ξ\xi-triad search, AMD Fibonacci structure, ξ\xi-ladder search, cross-system structural comparison
  • fibonacci_k1_anomaly.py — Belt-adjacent k=1k=1 anomaly investigation: coupling profile across Solar System (α×b3/2(1)\alpha \times b^{(1)}_{3/2}), block-diagonal decomposition, eigenmode isolation (participation entropy), Mars eigenmode pinning by Jupiter (93%99.8%93\% \to 99.8\%), coupling chain decay vs φn\varphi^n, cross-block coupling ratio =φ4.02= \varphi^{-4.02}, qualitative three-mechanism explanation
  • fibonacci_phi4_derivation.py — Quantitative φ4\varphi^4 derivation: four-factor logφ\log_\varphi budget decomposition (semi-major axis, η\eta-ratio (13/33)2(13/33)^2, inclination amplitudes, Laplace coefficients), algebraic 97%97\% contribution from F7/(F4×L5)F_7/(F_4 \times L_5), sensitivity analysis vs belt gap α\alpha, all cross-belt B-matrix ratios, eigenvector block structure, self-consistency check
  • fibonacci_cancellation_investigation.py — Investigation of the three non-algebraic logφ\log_\varphi factors: perturbation analysis (±20%\pm 20\% SMA, 10,000 trials, σ=2.6\sigma = 2.6), belt-gap scan showing BratioB_\text{ratio} crosses φ4\varphi^{-4} at Jupiter’s actual position, eigenvector-coupling constraint analysis, mirror-pair cancellation tests, demonstration that the 0.13-0.13 residual is KAM-selected (not structurally forced)
  • fibonacci_nbody_proper.py — Full N-body integration via REBOUND (WHFast, 10 Myr, Δt=4\Delta t = 4 days): osculating element extraction, proper eccentricity midpoints (87%87\% ladder spread vs model’s 0.014%0.014\%), proper inclination amplitudes (ecliptic vs invariable plane), BvW vs N-body extremes, instantaneous ladder spread over 10 Myr (min 3.75%3.75\%, never below 1%1\%), windowed midpoints, FFT eigenfrequency extraction, Mars eigenmode isolation in nonlinear regime
  • fibonacci_mercury_lucas.py — Mercury’s Lucas number b=11b = 11 investigation: additive chain analysis (bEarth+bSaturn=3+8=11=L5b_\text{Earth} + b_\text{Saturn} = 3 + 8 = 11 = L_5, non-adjacent Fibonacci sums \to Lucas), period fraction symmetry (Mercury (8,11)(8, 11) vs Mars (3,13)(3, 13) as belt-boundary duals), d=(21/13)×(13/2)d = (21/13) \times (13/2) KAM golden-ratio interpretation (21/13φ21/13 \approx \varphi at outermost mirror position k=4k = 4), 13/33=F7/(F4×L5)13/33 = F_7/(F_4 \times L_5) connection to φ4\varphi^4 belt barrier, eigenmode isolation analysis (Mercury 99.97%99.97\% pure, lowest participation entropy, Jupiter-dominated coupling 68.5%68.5\%), demonstration that b=bEarth+bSaturnb = b_\text{Earth} + b_\text{Saturn} is algebraic (Fibonacci chain) not physical coupling
  • fibonacci_311_deep.py — Deep investigation of why R311R \approx 311: Fibonacci primitive root prime census (600\leq 600, density 30%30\%), entry point α(311)=310\alpha(311) = 310 (Type 1, maximally efficient), continued fraction analysis (R=[310;1,4,1,2,1,2,128,...]R = [310; 1, 4, 1, 2, 1, 2, 128, ...], noble number test), secular eigenfrequency ratio search, physical constraints on FPR primes (Venus eccentricity range), Solar System super-period comparison, φ\varphi as primitive root of F311\mathbb{F}_{311} (verified: φmod311=59\varphi \bmod 311 = 59, ord(59)=310\text{ord}(59) = 310), Chirikov resonance overlap connection, quantum number modular arithmetic, two-layer synthesis (FPR necessary condition ++ formation-selected specific value)
  • fibonacci_j2000_eccentricity.py — J2000 eccentricity ladder investigation: BvW validity check (linear theory fails for Mercury/Mars), oscillation amplitude ratios (Δe/ebase\Delta e/e_\text{base}), ladder spread time series (±50\pm 50 Myr), per-planet d×ξd \times \xi tracking and correlation matrix (Venus–Earth anti-correlated r=0.577r = -0.577), Venus eccentricity cycle analysis, Earth midpoint self-consistency (optimal eE=0.01530e_E = 0.01530 matches model to 0.14%0.14\%), AMD analysis (Fibonacci ladder is AMD-costly, Mercury =51.4%= 51.4\% of inner AMD), Monte Carlo 100,000100{,}000 random AMD-matched distributions (p<105p < 10^{-5}), secular mode decomposition (all modes break ladder), demonstration that the eccentricity ladder is a formation constraint

Continue to Scientific Background for the physical context, or see Formulas for the complete calculation formulas.

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