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typicalLabPeriod_seconds
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IndisputableMonolith.Flight.GravityBridge on GitHub at line 62.
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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
81 T_dyn : ℝ -- Rotation period
82 τ0 : ℝ -- Recognition tick
83 α : ℝ -- ILG exponent
84 C_lag : ℝ -- Coupling constant
85 w_predicted : ℝ -- Predicted weight
86 h_w : w_predicted = 1 + C_lag * (Real.rpow (T_dyn / τ0) α - 1)
87
88/-- Construct a lab-scale prediction for a given device. -/
89def mkLabPrediction (T_dyn τ0 α C_lag : ℝ) : LabScalePrediction where
90 T_dyn := T_dyn
91 τ0 := τ0
92 α := α