vibe coding an orbital mechanics simulation to try out claude code
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1.4 KiB

Session Summary: Exact Position Burn Execution

Date: 2026-02-21

Changes Made

Implemented Option B from previous session's planning: exact position burn execution for true anomaly triggers.

Core Implementation

  • Added scheduled_dt field to Maneuver struct
  • Modified trigger logic to set scheduled_dt when crossing detected
  • Modified execution to propagate spacecraft to exact position before burn
  • Added wraparound handling for 2π→0 periapsis crossing
  • Added tracking array to prevent double-propagation in same frame

Files Modified

  • src/maneuver.h - Added scheduled_dt field
  • src/maneuver.cpp - Trigger logic, cleanup
  • src/simulation.cpp - Execution logic, tracking
  • src/config_loader.cpp - Initialize scheduled_dt
  • tests/test_periapsis_burn.cpp - Fixed tests
  • tests/test_periapsis_burn.toml - Fixed config
  • tests/test_maneuver_planning.cpp - Increased timeout
  • docs/planning/exact_position_burn_execution.md - Planning doc

Commits

680a8f4 Implement exact position burn execution for true anomaly triggers

Results

  • Net line count: +146 lines (207 additions, 61 deletions)
  • All 143 tests passing
  • Burns now execute at exact orbital position (within floating-point precision)

Remaining Issues

None - all tests passing, implementation complete.

Next Steps

Consider updating technical_reference.md to document the new scheduled_dt field in the Maneuver struct.