Add SIM_orbinit set03 (semi-latus rectum + true anomaly) Tier 3 coverage

[simnaut]

Summary

Extends SIM_orbinit Tier 3 coverage (#99 Bucket B) with the set03 orbital-init parameterization — JEOD SlrEccIncAscnodeArgperTanom (set = 3): semi-latus rectum (p) + true anomaly, plus eccentricity / inclination / ascending node / arg periapsis.

• RUN_0003 — ISS, Earth.inertial
• RUN_0103 — STS-114, Earth.inertial

Mirrors the set02 wave (PR #622): a new true_anomaly_element_state recipe helper + build_run_0003/0103 + run_0003/0103 in sim_orbinit_docker.rs, tier3 tests, bevy parity wrappers, and a new orbinit regen group entry in trick/generate_references.sh.

Key physics detail

JEOD's set03 branch selects shape = ShapeSemiLatusRectum, which skips the semi_latus_rectum = a·(1−e²) derivation (that runs only for sma-parameterized sets) and uses the deck's semi-latus rectum verbatim as elem.semiparam. The new converter init_from_semi_latus_rectum_true_anomaly therefore sets semiparam = p directly rather than round-tripping through a = p/(1−e²) — matching JEOD's arithmetic bit-closely. (dyn_body_init_orbit.cc:196-200, 285-321.)

Fixture schema change

OrbitalInitRecord / OrbitalInitData gain an optional semi_latus_rectum; semi_major_axis becomes Option (the two are mutually exclusive per JEOD set, and the parser requires exactly one). The .py parser and extract_body_init emit the new field; set03 is added to the SCENARIOS list for both ISS and STS-114. Existing sma-using call sites updated to .expect(...).

Observed t=0 errors vs JEOD (tolerances = 1.05× observed)

RUN	position	velocity
RUN_0003 (ISS)	5.21e-10 m	2.27e-13 m/s
RUN_0103 (STS)	1.40e-9 m	9.37e-13 m/s

Sub-nanometre agreement — consistent with the inertial set01/set02 RUNs.

pfix variants

RUN_0203/0303 (pfix set03) not included. The JEOD decks exist, but the set03 recipe helper would need its own frame-rotation branch (the set01 pfix path lives in a different helper); the inertial RUNs are the focused deliverable and pfix is a clean follow-up.

Verification

• cargo nextest run -p astrodyn_verif_jeod -E 'test(orbinit)' — 25 passed
• bevy_parity_orbinit_docker (incl. new run_0003/0103) + parity_coverage — 28 passed, superset invariant holds
• astrodyn_dynamics / astrodyn_math / astrodyn_verif_jeod_fixtures unit + Tier 2 — 488 passed
• invariant_coverage — passed
• cargo fmt --check clean; cargo clippy ... --tests -- -D warnings clean

🤖 Generated with Claude Code

[Copilot]

Pull request overview

Extends the SIM_orbinit Tier 3 JEOD parity suite to cover JEOD set03 (SlrEccIncAscnodeArgperTanom), initializing orbits from semi-latus rectum + true anomaly for ISS and STS-114 inertial runs, including fixture/schema updates and reference regeneration wiring.

Changes:

• Add set03 conversion path (init_from_semi_latus_rectum_true_anomaly) and corresponding verification scenario builders RUN_0003 / RUN_0103.
• Extend body-init fixture schema to support semi_latus_rectum and make semi_major_axis optional; regenerate ISS/STS fixtures and add new JEOD reference CSVs.
• Add Tier 3 tests + bevy parity wrappers, and include new runs in the Trick reference regeneration group.

Reviewed changes

Copilot reviewed 16 out of 16 changed files in this pull request and generated 2 comments.

Show a summary per file

File	Description
trick/generate_references.sh	Adds set03 RUN_0003/0103 to the orbinit reference regen group.
src/lib.rs	Re-exports the new set03 initializer from the top-level crate.
crates/astrodyn_verif_parity/tests/bevy_parity_orbinit_docker.rs	Adds parity tests for RUN_0003 and RUN_0103.
crates/astrodyn_verif_jeod/tests/tier3_sim_orbinit_docker.rs	Adds Tier 3 JEOD CSV validation tests for set03 inertial runs.
crates/astrodyn_verif_jeod/test_data/orbinit_0003_orbinit.csv	New JEOD reference output for RUN_0003.
crates/astrodyn_verif_jeod/test_data/orbinit_0103_orbinit.csv	New JEOD reference output for RUN_0103.
crates/astrodyn_verif_jeod/test_data/body_init/iss.json	Regenerated fixture with set03 entry and new nullable shape fields.
crates/astrodyn_verif_jeod/test_data/body_init/sts_114.json	Regenerated fixture with set03 entry and new nullable shape fields.
crates/astrodyn_verif_jeod/src/run_verification/sim_orbinit_docker.rs	Adds set03 recipe helper + builders and exposes run_0003/run_0103 verification cases.
crates/astrodyn_verif_jeod/src/bin/extract_body_init.rs	Emits the new semi_latus_rectum field and updates scenario extraction list.
crates/astrodyn_verif_jeod_fixtures/src/orbital_init.rs	Updates .py parser and data structs to support set03 semi-latus rectum input.
crates/astrodyn_verif_jeod_fixtures/src/body_init_fixtures.rs	Updates committed-JSON parser and record structs for nullable semi_major_axis and optional semi_latus_rectum.
crates/astrodyn_math/tests/jeod_validation.rs	Updates fixture consumers for semi_major_axis: Option<f64>.
crates/astrodyn_dynamics/tests/tier2_body_init.rs	Updates Tier 2 tests for semi_major_axis: Option<f64>.
crates/astrodyn_dynamics/src/lib.rs	Re-exports the new set03 initializer from astrodyn_dynamics.
crates/astrodyn_dynamics/src/body_init.rs	Implements init_from_semi_latus_rectum_true_anomaly and adds focused unit tests.

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