vibe coding an orbital mechanics simulation to try out claude code
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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
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6 months ago |
| .. |
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earth_circular.toml
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Migrate config system from space-separated to TOML format
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6 months ago |
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earth_mars_simple.toml
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removed unused velocity from test config
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6 months ago |
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hyperbolic_comet.toml
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Add hyperbolic orbit test case and configuration
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6 months ago |
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interplanetary_transfer.toml
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Phase 1: Enable root body transitions for patched conics
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6 months ago |
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maneuver_sequence.toml
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Implement maneuver planning system with config-based scheduled burns
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6 months ago |
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manual_root_transition.toml
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Phase 1: Enable root body transitions for patched conics
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6 months ago |
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mars_circular.toml
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Migrate config system from space-separated to TOML format
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6 months ago |
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mutual_soi_close.toml
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Add test suite for invalid parent assignment bugs
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6 months ago |
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parabolic_comet.toml
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Add parabolic orbit support and test case
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6 months ago |
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simple_root_transition.toml
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Phase 1: Enable root body transitions for patched conics
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6 months ago |
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soi_transition.toml
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Add simplified SOI transition test case
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6 months ago |
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solar_system.toml
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Fix Titan moon orbital stability
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6 months ago |
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spacecraft_test.toml
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Add local frame spacecraft maneuvering interface
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6 months ago |
