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def

typicalLabPeriod_seconds

definition
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module
IndisputableMonolith.Flight.GravityBridge
domain
Flight
line
62 · github
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IndisputableMonolith.Flight.GravityBridge on GitHub at line 62.

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All declarations in this module, on Recognition.

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formal source

  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