Implement first 7 priority functions for maneuver UI controls:
- add_maneuver_to_simulation(): Add maneuvers dynamically
- remove_maneuver_by_index(): Remove maneuvers from simulation
- create_maneuver(): Helper to construct maneuver structs
- get_burn_direction_name(): Get descriptive strings for directions
- preview_burn_result(): Preview orbital elements after burn
- calculate_hohmann_transfer(): Calculate optimal two-burn transfer
- validate_burn_parameters(): Validate burn parameters
See docs/planning/maneuver_ui_controls.md for full implementation plan.
- Switch spacecraft and bodies from RK4 to analytical propagation using propagate_orbital_elements()
- Fixed three bugs in hyperbolic orbit propagation (formula errors and insufficient Newton-Raphson iterations)
- Add orbital element reconstruction after burns and SOI transitions
- Zero energy drift for circular, elliptical, parabolic, and hyperbolic orbits
- All 132 tests passing (240,294 assertions)
Merge spacecraft management into simulation module:
- Move Spacecraft struct from maneuver.h to spacecraft.h
- Add spacecraft array to SimulationState (spacecraft, craft_count, max_craft)
- Remove separate SpacecraftState struct and related functions
- Update create_simulation() to require max_craft parameter
- Move spacecraft update logic into update_simulation()
- Make load_spacecraft_config() internal helper, called by load_system_config()
- Update all test files to use new API with 3-parameter create_simulation()
- Handle max_craft=0 case gracefully (no spacecraft allocation)
Test results: 26/27 passing (1 pre-existing SOI test unrelated to changes)
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)
cinnaboot