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rotationPeriod
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IndisputableMonolith.Flight.GravityBridge on GitHub at line 50.
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47/-! ## Device Dynamical Timescale -/
48
49/-- A rotating device with angular velocity ω has period T = 2π/ω. -/
50def rotationPeriod (ω : ℝ) (hω : ω ≠ 0) : ℝ := 2 * Real.pi / ω
51
52/-- The dynamical timescale of a φ-spiral rotor is its rotation period. -/
53def deviceDynamicalTime (ω : ℝ) (hω : ω ≠ 0) : ℝ := rotationPeriod ω hω
54
55/-! ## ILG Weight at Lab Scales -/
56
57/-- Reference recognition tick τ₀ in seconds (from RS constants).
58 τ₀ = 1/(8 ln φ) in natural units ≈ 7.3 × 10⁻¹⁵ s. -/
59def tau0_seconds : ℝ := 7.3e-15
60
61/-- A typical lab rotation period (e.g., 1000 RPM = 0.06 s). -/
62def typicalLabPeriod_seconds : ℝ := 0.06
63
64/-- Ratio T_dyn/τ₀ for typical lab device. This is enormous (~10¹³). -/
65def labScaleRatio : ℝ := typicalLabPeriod_seconds / tau0_seconds
66
67/-- The ILG exponent α = (1 - φ⁻¹)/2 ≈ 0.191.
68 Using the RS constant φ = (1 + √5)/2. -/
69def ilg_alpha : ℝ := (1 - 1/phi) / 2
70
71/-- Lab-scale weight deviation: for α ≈ 0.191 and ratio ≈ 10¹³,
72 the term (T_dyn/τ₀)^α ≈ (10¹³)^0.191 ≈ 10^2.5 ≈ 316.
73
74 However, C_lag is typically 10⁻³ to 10⁻⁵ for consistency with
75 solar system tests. So the deviation is:
76 w - 1 = C_lag * 315 ≈ 0.3 (at C_lag = 10⁻³)
77
78 This is a TESTABLE prediction if C_lag is not too small.
79-/
80structure LabScalePrediction where