claudes_game

0 Tags

1.9 MiB

Author	SHA1	Message	Date
cinnaboot	fe6f9dcd5e	remove extra decorative comment blocks in python scripts	2 months ago
cinnaboot	1e4ed912d2	refactor: test_parabolic_orbit with SI-unit precalc and tightened tolerances - Merge initial conditions check into single SCENARIO - Tighten energy check to relative error (1e-10) vs KE - Replace qualitative checks with quantitative WithinAbs assertions - Use named tolerance constants throughout fixture - Update precalc_parabolic_orbit.py to output SI units (m, m/s) - Precalculate expected values with full precision from Python - Python and C++ produce identical results in SI units - Add semi_latus_rectum support in sim_engine.py for parabolic orbits	2 months ago
cinnaboot	b333a1745f	refactor test_maneuvers: add spacecraft struct to sim_engine, rewrite tests - Add Spacecraft dataclass, BurnDirection enum, and burn functions to sim_engine.py - Add spacecraft config loading, initialization, and propagation to Simulator - Convert TOML config to TOML 1.0 inline table syntax - Rewrite test_maneuvers.cpp as 1 SCENARIO with 6 SECTIONs (proper fixture reuse) - Use local-frame distances for burn tests (global dominated by Earth-Sun distance) - Tighten propagation stability checks: distance drift < 0.01%, a drift < 0.01%, e preserved within 1e-6 - Remove old test files	2 months ago
cinnaboot	30b8127a55	feat: add sim_engine.py and test_orbital_period.py for precalculation - sim_engine.py: generic orbital mechanics simulator with RK4 + analytical propagation, used to verify C++ test expected values - test_orbital_period.py: precalculation script with safety timeout for measuring Earth/Mars orbital periods and direction test values - Remove SOI transition logic (buggy in both Python and C++ versions) - Use dataclasses.replace() for immutable state updates - Support single-line TOML inline tables via tomllib	2 months ago

4 Commits (93b7252494aea8e4782764f4919df0959e104e88)