vibe coding an orbital mechanics simulation to try out claude code

You can not select more than 25 topics Topics must start with a letter or number, can include dashes ('-') and can be up to 35 characters long.

Tree: 5ebac26118

main

test-refactor

Branches Tags

${ item.name }

Create tag ${ searchTerm }

Create branch ${ searchTerm }

from '5ebac26118'

${ noResults }

claudes_game/tests

History

cinnaboot 5ebac26118 Implement config-based spacecraft with LEO initialization and impulse burn ... - Add spacecraft body to earth_mars_simple.toml config file - Implement initialize_spacecraft_leo() to set circular LEO at 200km altitude - Implement apply_transfer_burn() for Hohmann transfer impulse burn - Implement calculate_phase_angle() for launch window verification - Add comprehensive test case with SOI transition tracking - Preserve debug printf statements from main branch investigation - LEO initialization verified: position, velocity, energy all correct - Issue identified: delta-v calculation doesn't account for spacecraft LEO phase - Test completes 8/9 assertions (fails post-burn energy check) - Session documented in docs/leospacecraft_impulse_burn_plan.md Next: Fix apply_transfer_burn() to use vector-based delta-v instead of magnitude-based		7 months ago
..
configs	Implement config-based spacecraft with LEO initialization and impulse burn	7 months ago
test_energy.cpp	Rename bodies.h/cpp to simulation.h/cpp	8 months ago
test_hohmann_transfer.cpp	Implement config-based spacecraft with LEO initialization and impulse burn	7 months ago
test_hyperbolic_orbit.cpp	Add hyperbolic orbit test case and configuration	7 months ago
test_integration.cpp	Add Catch2 testing and implement RK4 integration	8 months ago
test_main.cpp	Add Catch2 testing and implement RK4 integration	8 months ago
test_mission_planning.cpp	Phase 1-3: Implement mission planning module for Hohmann transfers	7 months ago
test_moon_orbits.cpp	Add moon orbit test suite and fix solar system config	8 months ago
test_orbital_period.cpp	Rename bodies.h/cpp to simulation.h/cpp	8 months ago
test_parabolic_orbit.cpp	Add parabolic orbit support and test case	7 months ago
test_root_body_transitions.cpp	Phase 1: Enable root body transitions for patched conics	7 months ago
test_soi_transition.cpp	Simplify find_dominant_body to remove hysteresis	7 months ago