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test-refactor

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5 Commits (6c28eb1560d2b106efbe09e3e70d4aa2d6222f29)

Author	SHA1	Message	Date
cinnaboot	3bbac86ca5	refactor test_maneuver_planning: SCENARIO/SECTION pattern, quantitative assertions, TOML 1.0 config, precalc script	3 weeks ago
cinnaboot	2a86e7093a	use old_tests/ while refactoring tests	2 months ago
cinnaboot	4b77ad6ff7	Fix true anomaly trigger at periapsis ... Swap order in update_simulation() to check maneuvers before physics update. This ensures triggers fire at the correct position instead of after the spacecraft has moved past the trigger point. Also fix test config to avoid interference between time-based and true anomaly triggers.	5 months ago
cinnaboot	b221251787	Remove altitude parameter to fix spacecraft initialization bug ... - Remove altitude convenience parameter from body and spacecraft config parsing - Update test configs to use explicit semi_major_axis instead of altitude - Remove buggy post-processing loop that added parent radius to all spacecraft - Result: Semi-major axis now used as-is (correct behavior) - Test results: Molniya position tests now pass (was failing by 1-11M meters) - Documentation: Remove altitude references from technical reference - Planning: Document bug fix decision and implementation details Changes: - src/config_loader.cpp: Remove altitude parsing and post-processing - tests/test_maneuver_planning.toml: Use semi_major_axis = 6.771e6 - tests/test_maneuvers.toml: Use semi_major_axis = 6.771e6 - tests/test_orbit_rendering.toml: Use semi_major_axis = 6.771e6 - docs/technical_reference.md: Remove altitude documentation - docs/planning/molniya-orbit-test-plan.md: Document bug fix approach	5 months ago
cinnaboot	f79ae5ac84	reorganize test configs: 1:1 mapping with test files ... - Move all configs from tests/configs/ to tests/ - Rename configs to match test filenames (test_NAME.toml) - Remove unused configs (earth_mars_simple, simple_root_transition, interplanetary_transfer) - Combine earth_circular and mars_circular into test_orbital_period.toml - Duplicate earth_circular.toml as test_energy.toml - Remove invalid parent test case from test_invalid_parent_assignment.cpp - Update all test files to reference new config paths - Delete tests/configs/ directory	6 months ago
cinnaboot	4c8050be84	fix missing commas in orbit TOML blocks	6 months ago
cinnaboot	64f20ef309	Phase 5: Update all test configs to new orbit table format	6 months ago
cinnaboot	ce35c618d6	Implement maneuver planning system with config-based scheduled burns ... Add maneuver planning and execution system to SimulationState: **Data Structures:** - Add TriggerType enum (TIME, TRUE_ANOMALY) - Add Maneuver struct with burn parameters, trigger conditions, execution state - Add maneuver array to SimulationState (maneuvers, maneuver_count, max_maneuvers) - Update create_simulation() to accept max_maneuvers parameter **Config File Format:** - [[maneuvers]] sections with name, spacecraft_name, trigger_type, trigger_value, direction, delta_v - Validate spacecraft_name exists and maneuver names are unique - Parse trigger_type string -> enum - Parse direction string -> BurnDirection enum **Execution System:** - check_maneuver_trigger() evaluates TIME and TRUE_ANOMALY conditions - TIME trigger: sim->time >= trigger_value - TRUE_ANOMALY trigger: calculate orbital true anomaly from position/velocity - execute_maneuver() applies delta-v using apply_impulsive_burn() - Maneuvers execute in update_simulation() after spacecraft physics - Global coordinates computed AFTER maneuvers to preserve burn effects **Test Coverage (5 tests, 26 assertions):** - Maneuver loading from config - Time-based trigger executes at correct time - True anomaly trigger executes at correct angle - Maneuvers only execute once - Duplicate maneuver names fail config load **API Changes:** - create_simulation(int max_bodies, int max_craft, int max_maneuvers, double time_step) - Updated all existing test files to use new signature Test results: 5/5 maneuver tests passing Documentation: docs/maneuver_planning_plan.md with full design specification	6 months ago
cinnaboot	2f7ae72bf0	Add local frame spacecraft maneuvering interface ... Add basic maneuvering API for spacecraft with impulsive delta-v burns in local frame: - Add vec3_dot() function to physics module - Create Spacecraft struct and SpacecraftState for separate spacecraft management - Implement 6 burn directions: prograde, retrograde, normal, anti-normal, radial in/out - Add RK4 propagation for spacecraft with update_spacecraft() - Extend config loader to parse [[spacecraft]] TOML sections - Add 6 test cases verifying burn physics and propagation stability - Rename old mission_planning module to _old for future reference Test results: 26/27 passing (1 pre-existing SOI test unrelated to changes)	6 months ago
cinnaboot	1ac7e359a4	Migrate config system from space-separated to TOML format ... - Add tomlc17 library as git submodule - Update Makefile to build tomlc17.c with C compiler - Replace config_loader.cpp with TOML-based implementation - Add helper functions for parsing TOML tables (position, color) - Convert all 5 config files from .txt to .toml format: * configs/solar_system.toml - full solar system with planets and moons * configs/example_binary_star.toml - binary star system * configs/test_simple.toml - various orbit types for testing * tests/configs/earth_circular.toml - Earth orbit test * tests/configs/mars_circular.toml - Mars orbit test - Update all test files to reference .toml extensions - Remove old .txt config files (maintain compatibility) - Support both INT64 and FP64 TOML values (tomlc17 type flexibility) - All automated tests pass with new TOML format Claude	6 months ago