Interface to external-field coupling

An input interface for the later Gravity module; background-field and orbital equations are outside this module.

Theory · DERIVEDEquation version 1.0.0

Based on the final manuscript · Chapter 2

U_{\mathrm{ext}}=m_0\Psi_{\mathrm{ext}}=\frac12m_0c^2(X_{\mathrm{ext}}-1),\qquad\mathbf F_g=-\nabla U_{\mathrm{ext}}=m_0\mathbf g_X

An input interface for the later Gravity module; background-field and orbital equations are outside this module.
Chapter reference: Final collected manuscript · Chapter 2 §III.5 (2.24d) · ASD-BOOK-ddbade997b45

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Final collected manuscript · Chapter 2 §III.5 (2.24d)

An input interface for the later Gravity module; background-field and orbital equations are outside this module.

Conditions retained in this adoption

Uniform background, fixed internal state, 0≤v<c and no net radiation.
The LVE directional law and inertial angular weight are separate inputs.
m₀=C_m m_def; adopt C_m=1 and universal mass normalization.

Specific unresolved source issues

The microscopic core profile, inertial weight and four mass responses still require one common structural solution.

Source locators: p0669 · p0671 · p0672 · p0674 · p0675 · p0936 · 最终合订稿 · 第二章 §三.5 (2.24d)

Manuscript SHA-256: ddbade997b45913248e588953b1d27ccb9c7c206c3c8d992d3aef2364a64836e

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Previous source, retained as history

FND-3dde8d8e081d · 第二章 §三，(2.24d), PDF p. 10

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