ANISOTROPIC SPACE DYNAMICS · CANONICAL THEORY

Dynamics · Inertia and Momentum

Trace the near-core density deficit, axial LVE gain, inertial constitutive closure and angular integration of total momentum.

Based on the final manuscript · Chapter 2

TheoryTheory · DERIVEDReviewMathematical review · CONDITIONALEvidenceEvidence · UNTESTEDCanonicalYesStatus, review and sources

ASD interprets inertia as the directional reconstruction response required to change the joint motion of a topological core and its accompanying spatial field. LVE supplies directional scales; the inertial weight specifies how directions contribute to total momentum. With the stated closure and normalization, angular integration gives p=m0γv\mathbf p=m_0\gamma\mathbf v. The web notation ϕ\phi denotes the manuscript motion angle χ\chi in (2.10)–(2.12), while the integration azimuth is α\alpha.

01Premises and quantities · Starting Assumptions

This page retains Chapter 2’s chain from core structure to momentum. A1–A4 are website premise indices. Upstream LVE keeps its v1.1 conditional mathematical review; using it in dynamics does not make it unconditional.

A1 · Assumption

Treat the core and accompanying field jointly

Consider a localized material structure in a uniform background, with fixed internal state and common translational velocity v\mathbf v. ρ0\rho_0 is the calibrated background volume density; qρq_\rho is the near-core volume-density ratio. The effective-core deficit integral must be finite and give positive m0m_0. Source: Chapter 2, §III, final manuscript §III.

A2 · Assumption

Use the effective core and mass normalization

Define ReffR_{\mathrm{eff}} from the equal-deficit volume. Adopt m0=Cmmdefm_0=C_m m_{\mathrm{def}} with Cm=1C_m=1. ReffR_{\mathrm{eff}} is an effective integration radius, not automatically a measured geometric particle radius. Source: Eqs. (2.8)–(2.9) and adjacent text.

A3 · Assumption

Adopt the LVE directional scale

Use Chapter 1’s K(ϕ)=γ(1−βcos⁡ϕ)K(\phi)=\gamma(1-\beta\cos\phi), with 0≤β<10\leq\beta<1. ϕ\phi is measured relative to velocity, and KK describes ASD true-length relations. Source: Eq. (2.10); LVE derivation and review.

A4 · Assumption

Adopt inertial closure and momentum density

Use the symmetric gain of inverse axial scales as the overall inertial gain and the lowest angular harmonic for the forward/backward bias. Set ρI=ρ0γ(1+βcos⁡ϕ)\rho_I=\rho_0\gamma(1+\beta\cos\phi) and momentum density π=ρIv\boldsymbol\pi=\rho_I\mathbf v. Chapter 2 explicitly introduces this constitutive relation; it is not a geometric identity of LVE. Source: Eqs. (2.11)–(2.12).

02Near-core mass and effective volume · Mass and Effective Volume

ASD-WEB-DYN-002
mdef=ρ0∫D[1−qρ(x)] dV0m_{\mathrm{def}}=\rho_0\int_{\mathcal D}[1-q_\rho(\mathbf x)]\,\mathrm dV_0

Constitutive input
q_ρ is a near-core volume-density ratio and D an effective core domain; the far-field line-density coefficient Φ is a different quantity.
Chapter reference: Final collected manuscript · Chapter 2 §III.1 (2.8) · ASD-BOOK-ddbade997b45

ASD-WEB-DYN-003
Veff=∫D(1−qρ) dV0=4πReff33,m0=Cmmdef,Cm=1.\begin{aligned}V_{\mathrm{eff}}&=\int_{\mathcal D}(1-q_\rho)\,\mathrm dV_0=\frac{4\pi R_{\mathrm{eff}}^3}{3},\\m_0&=C_m m_{\mathrm{def}},\qquad C_m=1.\end{aligned}

Normalization
R_eff is the equal-deficit-volume radius; C_m=1 is the mass normalization adopted in this chapter.
Chapter reference: Final collected manuscript · Chapter 2 §III.1 (2.9) and normalization · ASD-BOOK-ddbade997b45

It follows that m0=ρ0Veff=4πρ0Reff3/3m_0=\rho_0V_{\mathrm{eff}}=4\pi\rho_0R_{\mathrm{eff}}^3/3. The normalization in this equality must remain attached to the momentum result.

Chapter 2’s far-field Φ\Phi is a line-density coefficient, whereas qρq_\rho is a near-core volume-density ratio. They are not interchangeable. Inserting an external 1/r1/r line field directly into an all-space volume-deficit integral is not the construction of Eq. (2.8); extending the domain requires a separate convergence argument.

03LVE and axial gain · Directional Scale

ASD-WEB-DYN-004
L′=LK(ϕ),K(ϕ)=γ(1−βcos⁡ϕ),β=vc,γ=(1−β2)−1/2L^\prime=LK(\phi),\quad K(\phi)=\gamma(1-\beta\cos\phi),\quad\beta=\frac vc,\quad\gamma=(1-\beta^2)^{-1/2}

Upstream input
Retain Chapter 1’s directional true-length interpretation and mathematical review conditions; χ is the angle to velocity.
Chapter reference: Final collected manuscript · Chapter 2 §III.2 (2.10) · ASD-BOOK-ddbade997b45

Set cos⁡ϕ=+1,−1\cos\phi=+1,-1 along the forward and backward axes:

ASD-WEB-DYN-005
K+=γ(1−β),K−=γ(1+β),K+K−=1,K+−1+K−−12=γK_+=\gamma(1-\beta),\quad K_-=\gamma(1+\beta),\quad K_+K_-=1,\quad\frac{K_+^{-1}+K_-^{-1}}2=\gamma

Mathematical result
This is an identity for two axial factors; a full inertial angular distribution requires an additional constitutive input.
Chapter reference: Final collected manuscript · Chapter 2 §III.2 (2.10a) · ASD-BOOK-ddbade997b45

The intermediate algebra is K+K−=γ2(1−β2)=1K_+K_-=\gamma^2(1-\beta^2)=1. Hence K+−1=K−K_+^{-1}=K_- and K−−1=K+K_-^{-1}=K_+, whose average is γ\gamma. Up to this point, the result concerns the algebra of two axial factors.

04Inertial angular distribution · Constitutive Closure

Constitutive Input

From axial gain to a full angular distribution

Interpreting the average as the overall inertial gain, and adopting the lowest angular harmonic 1+βcos⁡ϕ1+\beta\cos\phi for the bias, gives the manuscript’s closure:

ASD-WEB-DYN-006
ρI(ϕ)=ρ0γ(1+βcos⁡ϕ),14π∫ρI dΩang=ρ0γ\rho_I(\phi)=\rho_0\gamma(1+\beta\cos\phi),\qquad\frac1{4\pi}\int\rho_I\,\mathrm d\Omega_{\mathrm{ang}}=\rho_0\gamma

Constitutive input
The lowest angular bias and mean gain are additional inputs; ρ_I is not generally ρ₀/K(χ).
Chapter reference: Final collected manuscript · Chapter 2 §III.2 (2.11) · ASD-BOOK-ddbade997b45

ρI\rho_I has density dimensions and is an inertial weight density, not the actual volume density at every point. In general directions, K(ϕ)−1≠γ(1+βcos⁡ϕ)K(\phi)^{-1}\ne\gamma(1+\beta\cos\phi). At ϕ=π/2\phi=\pi/2, for example, these are 1/γ1/\gamma and γ\gamma. Equation (2.11) therefore cannot silently be derived by identifying density with inverse length in every direction.

05Total momentum and intermediate steps · Momentum Integration

ASD-WEB-DYN-007
p=v∫0Reffr2 dr∫02πdα∫0πρI(ϕ)sin⁡ϕ dϕ\mathbf p=\mathbf v\int_0^{R_{\mathrm{eff}}}r^2\,dr\int_0^{2\pi}d\alpha\int_0^\pi\rho_I(\phi)\sin\phi\,d\phi

Constitutive input
The integral uses the chapter’s effective core and common translational velocity; microscopic nonuniform structure still needs matching.
Chapter reference: Final collected manuscript · Chapter 2 §III.2 (2.12) · ASD-BOOK-ddbade997b45

In the chapter’s effective construction, ρI\rho_I retains only angular dependence. Integrating term by term:

∫0πsin⁡ϕ dϕ=2,∫0πcos⁡ϕsin⁡ϕ dϕ=0.\int_0^\pi\sin\phi\,d\phi=2, \qquad \int_0^\pi\cos\phi\sin\phi\,d\phi=0.

Consequently,

∫02πdα∫0πρIsin⁡ϕ dϕ=4πρ0γ,∫0Reffr2dr=Reff33.\int_0^{2\pi}d\alpha\int_0^\pi\rho_I\sin\phi\,d\phi =4\pi\rho_0\gamma, \qquad \int_0^{R_{\mathrm{eff}}}r^2dr=\frac{R_{\mathrm{eff}}^3}{3}.

Multiplying and applying A2 yields:

ASD-WEB-DYN-008
p=4π3ρ0Reff3γv=m0γv,p=m0γv\mathbf p=\frac{4\pi}{3}\rho_0R_{\mathrm{eff}}^3\gamma\mathbf v=m_0\gamma\mathbf v,\qquad p=m_0\gamma v

Mathematical result
The odd angular term integrates to zero; the result uses the stated mass normalization.
Chapter reference: Final collected manuscript · Chapter 2 §III.2 (2.13)—(2.14) · ASD-BOOK-ddbade997b45

The odd directional term contributes zero to this integral. The mean gain γ\gamma contributes to the total momentum. These steps retain the algebra needed between Eqs. (2.12) and (2.14).

06Structural meaning · Physical Interpretation

ASD interprets γ\gamma as the inertial gain of the moving spatial structure. Changing the motion of a core and its accompanying structure changes the momentum of the joint system. The matching mathematical form is not interpreted as a change of rest mass caused by a time-flow rate.

Reconfiguration response is not dissipative drag during uniform motion. Maintaining free uniform motion costs no continuous work in this construction; work is associated with changing the state.

07Validity and consistency · Domain and Checks

  • Rest limit: As β→0\beta\to0, ρI→ρ0\rho_I\to\rho_0, γ→1\gamma\to1 and p→m0vp\to m_0v.
  • Dimensions and positivity: ρI\rho_I is mass per volume; the integral has mass-times-speed dimensions. For β<1\beta<1, 1+βcos⁡ϕ>01+\beta\cos\phi>0.
  • Symmetry: The angular mean of the directional bias vanishes, while v\mathbf v still determines the direction of total motion.
  • Domain: Do not cross v=cv=c or apply the fixed-state m0m_0 to radiation or internal excitation without extending the model.

A common mean gain does not uniquely fix an angular distribution. Higher terms with zero angular mean can leave this integral unchanged; spatial dynamics must select the actual profile. This check does not replace the manuscript’s lowest-order constitutive choice.

08Mathematical review and inputs · Review and Dependencies

  1. LVE input: Retain the upstream review of A5’s pairing and mapping conditions.
  2. Constitutive origin: Derive the gain and angular distribution of Eq. (2.11) from closed spatial dynamics and a stable core solution, beyond the axial identity.
  3. Core matching: Relate qρq_\rho, the effective-core integral and a real nonuniform structure, and establish a finite mass integral.
  4. Common normalization: A single structural solution must test whether Cm=1C_m=1, E0=m0c2E_0=m_0c^2 and the universal coupling of Eq. (2.24c) hold simultaneously.

OP-DYN-01 (Chinese) · Chinese original collects these tasks. The angular integration is closed under A1–A4. Mathematical review remains CONDITIONAL to preserve the physical inputs.

09Sources and continuation · Sources

This page corresponds to Chapter 2 §III, final manuscript §III. Continue to Force and Work for dp/dtd\mathbf p/dt, or Energy for ∫v⋅dp\int\mathbf v\cdot d\mathbf p.

On this page
STATUS & REVIEW
Theory StatusTheory · DERIVED
Mathematical ReviewMathematical review · CONDITIONAL
Overall Evidence StatusEvidence · UNTESTED
Canonical ASDYes · canonical theory baselinePreface · Chapters 1–2
Mathematical Review Note

Momentum follows after the inertial constitutive closure; total energy additionally uses E₀ = m₀c². These inputs remain explicit and require microscopic matching.

Read the formal review items
Adopted source, conditions and previous versions

§III.1—2 (2.8)—(2.14)

Core–accompanying-field inertial constitution, momentum integration, inverse force response and energy; retain correct existing derivations.

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: p0610 · p0613 · p0615 · p0620 · p0624 · p0628 · p0630 · p0936

Manuscript SHA-256: ddbade997b45913248e588953b1d27ccb9c7c206c3c8d992d3aef2364a64836e

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FND-3dde8d8e081d · Chapter 2, §III, Eqs. (2.8)–(2.14), PDF pp. 6–8; Chapter 1 LVE is an input

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Chapter 2 · §III.1—2 (2.8)—(2.14)

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ASD: Dynamics · Inertia and Momentum. ASD-DOC-EN-THEORY-DYNAMICS-MOMENTUM. Version 1.0.0; 2026-10-24. https://asd-physics.org/en/theory/dynamics/momentum. §III.1—2 (2.8)—(2.14). Source ASD-BOOK-ddbade997b45.

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