Add SIM_orbinit set02 (mean-anomaly) RUN_0002/0102 (#99)

[simnaut]

Summary

Extends SIM_orbinit Tier 3 coverage (5/46 → 7/46) with the mean-anomaly orbital-init parameterization — JEOD DynBodyInitOrbit::SmaEccIncAscnodeArgperMeanAnomaly ("set02"), distinct from the covered set01 time-periapsis path. Adds RUN_0002 (ISS) and RUN_0102 (STS-114), both Earth.inertial.

This is a genuine Tier-3 trajectory wave: orbital-element → Cartesian init → Simulation::step() propagation, with full bevy↔runner parity.

• Both set02 runs are driven from committed body-init fixtures (test_data/body_init/{iss,sts_114}.json), loaded via load_orbital_init and converted by the new mean_anomaly_element_state recipe helper, which reads the fixture's mean_anomaly field directly (mirroring how set01 loads and derives M from time_periapsis). No orbital elements are hardcoded at the call site.
• tier3 tests assert our element→Cartesian init reproduces JEOD's t=0 logged state (pos err ~1–6e-9 m, vel ~e-12 m/s — FP noise; tolerances 1.05× observed), then propagate.
• bevy_parity wrappers assert runner≡bevy bit-identity at every synthetic checkpoint.
• Regen group extended + 2 reference CSVs committed.

Fixture / conversion changes (addressing review)

• extract_body_init now extracts trans_Orbit_inertial_body_set02 for STS_114 as well as ISS; sts_114.json regenerated with the new entry.
• The fixtures parser's degree→radian conversion is aligned from val * PI / 180.0 (two roundings) to f64::to_radians() (single rounding). Both fixtures regenerated — the only value deltas are 1-ULP shifts in a few degree-derived angles (machine-epsilon; ~1e-15 relative). Both files now carry a real generated_utc.
• Affected orbinit Tier 3 tolerances re-derived to 1.05× observed: RUN_0001 → 6.56e-9 / 6.50e-12; RUN_0101 velocity tightened 1.93e-12 → 2.39e-13 (more-accurate conversion). RUN_0002/RUN_0102 land on the original observed tolerances.

Verification

• All 7 tier3_orbinit_docker_* + 7 bevy_parity_orbinit_docker_* pass; full fixture-consumer suites (dynamics/math/fixtures) green.
• cargo fmt --check + cargo clippy --workspace --tests -- -D warnings clean.

Next in the orbinit set

set03 (true-anomaly via semi-latus-rectum) maps onto init_from_orbital_elements; sets 04–11 (altitude apo/peri, arg-latitude + radial-vel) need small element-conversion additions. Tracked under #99 Bucket B.

🤖 Generated with Claude Code

[Copilot]

Pull request overview

Extends the SIM_orbinit Tier 3 verification matrix by adding two new Docker-backed runs that validate the set02 mean-anomaly orbital-element initialization path (ISS RUN_0002 and STS-114 RUN_0102) against JEOD’s logged t=0 state and also assert runner↔bevy bit-parity at synthetic checkpoints.

Changes:

• Add two new SIM_orbinit Docker verification cases (run_0002, run_0102) that initialize from set02 mean anomaly elements.
• Add Tier 3 JEOD cross-validation tests and bevy parity wrappers for the two new runs.
• Extend reference generation + commit two new JEOD reference CSVs for RUN_0002 and RUN_0102.

Reviewed changes

Copilot reviewed 6 out of 6 changed files in this pull request and generated 2 comments.

Show a summary per file

File	Description
trick/generate_references.sh	Adds RUN_0002/0102 to the SIM_orbinit reference-generation group.
crates/astrodyn_verif_parity/tests/bevy_parity_orbinit_docker.rs	Adds parity tests for the two new orbinit Docker runs.
crates/astrodyn_verif_jeod/tests/tier3_sim_orbinit_docker.rs	Adds Tier 3 assertions against JEOD t=0 for RUN_0002/0102 with tight tolerances.
crates/astrodyn_verif_jeod/test_data/orbinit_0002_orbinit.csv	Adds JEOD t=0 reference record for RUN_0002.
crates/astrodyn_verif_jeod/test_data/orbinit_0102_orbinit.csv	Adds JEOD t=0 reference record for RUN_0102.
crates/astrodyn_verif_jeod/src/run_verification/sim_orbinit_docker.rs	Introduces set02 mean-anomaly state construction and exports new verification cases.

---

💡 Add Copilot custom instructions for smarter, more guided reviews. Learn how to get started.