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test-refactor

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4 Commits (0d2be152856f4bee55c9b93fbc5054024f5ad0ba)

Author	SHA1	Message	Date
cinnaboot	680a8f4a90	Implement exact position burn execution for true anomaly triggers ... - Add scheduled_dt field to Maneuver struct for precise timing - Propagate spacecraft to exact trigger position before burn execution - Handle 2π→0 wraparound in trigger crossing detection - Add spacecraft tracking to prevent double-propagation in same frame - Fix test configs and tolerances for new behavior All 143 tests passing.	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	dbf9231f14	fix whitespace	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