Tree: 9fd6b25658

main

test-refactor

Branches Tags

${ item.name }

Create tag ${ searchTerm }

Create branch ${ searchTerm }

from '9fd6b25658'

${ noResults }

Commit Graph

3 Commits (9fd6b2565853a2c1640fb661dea47ed0d7fe65da)

Author	SHA1	Message	Date
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