claudes_game

Author	SHA1	Message	Date
cinnaboot	c023723aff	add session summary: test config reorganization and physics test coverage	6 months ago
cinnaboot	f25bd32e63	add session summary for config validation refactoring	6 months ago
cinnaboot	ddf30594d2	add session summary	6 months ago
cinnaboot	aaeb4b1b8d	add session summary	6 months ago
cinnaboot	95a5383266	Session: Spacecraft rendering and billboard refactor - Initial spacecraft rendering with wireframe spheres - Maneuver markers as colored cubes - Full UI integration (object list, info panel, maneuver list) - Refactored to proper billboard rendering - Programmatic texture generation (no external assets) - Directional rotation showing velocity vector - Upgraded maneuver markers to directional arrows - Lazy texture loading and proper cleanup	6 months ago
cinnaboot	10ae07fdf6	Session: Documentation restructuring and organization Consolidated documentation structure: - Merged duplicate coordinate frame sections into single coherent section - Extracted rendering system to docs/rendering.md (308 lines) - Extracted future work roadmap to docs/future_work.md (258 lines) - Renamed implementation_plan.md → technical_reference.md for clarity - Added spacecraft and maneuver config loader documentation - Updated all cross-references (README.md, AGENTS.md, opencode.json) - Removed obsolete AccelerationContext struct reference Total: +646 lines documentation, 2 new files, 1 renamed	6 months ago
cinnaboot	4699b08a94	Session: Local frame spacecraft maneuvering with planning system Implemented maneuver planning system for spacecraft with time-based and true anomaly triggers: New Module: src/maneuver - TriggerType enum (TIME, TRUE_ANOMALY) - Maneuver struct with burn parameters, trigger conditions, execution state - Burn execution: apply_impulsive_burn() for 6 directions - Trigger checking: check_maneuver_trigger() with orbital calculations Simulation State Integration: - Added maneuver array to SimulationState - create_simulation() now takes max_maneuvers parameter - Maneuvers execute automatically in update_simulation() - Config loading handles [[maneuvers]] sections Config File Support: - [[maneuvers]] sections with name, spacecraft_name, trigger_type, trigger_value, direction, delta_v - Validate spacecraft exists before loading - Validate maneuver names are unique - Parse trigger_type and direction strings to enums Code Quality: - Refactored update_simulation into 5 helper functions - Single responsibility per function - Cleaner, more readable code Test Coverage: - 5 new tests for maneuver planning (26 assertions) - Config loading validation - Time-based trigger execution - True anomaly trigger execution - Single execution guarantee - Duplicate name validation Test Results: 5/5 tests passing (100%) - All existing tests continue to pass Documentation: - docs/maneuver_planning_plan.md - Full design specification - docs/refactor_update_simulation.md - Refactoring plan Total Changes: - Files: 18 created/modified - Net: +823 lines of well-documented, tested code	6 months ago
cinnaboot	1795caabd1	add session summary for hohmann transfer work	6 months ago
cinnaboot	e73f8876d8	Add session summary: Invalid Parent Assignment Bug Resolution Session: January 20, 2026 (~2 hours) Branch: mission-planning Goals Achieved: 1. Diagnosed spacecraft initialization bug from mission_planning.md FIXME 2. Created comprehensive test suite with 4 test cases 3. Implemented config validation for parent-child distances 4. Fixed spacecraft position in earth_mars_simple.toml (LEO altitude) 5. Updated test 3 to use radius-based validation 6. Updated documentation to reflect resolution status Results: - Tests 1-3 now pass (Earth→Spacecraft, Mass Hierarchy, Config Validation) - Test 4 fails as expected (Mutual SOI edge case - separate issue) - FIXME bug from mission_planning.md now resolved Files Created: - docs/test_plan_invalid_parent_assignment.md (+185 lines) - tests/test_invalid_parent_assignment.cpp (+177 lines) - tests/configs/mutual_soi_close.toml (+34 lines) - docs/session_summaries/2026-01-20-invalid-parent-assignment-bug-resolution.md (+252 lines) Files Modified: - src/config_loader.cpp (+20 lines) - Config validation - tests/configs/earth_mars_simple.toml (position corrected) - docs/mission_planning.md (+7/-14 lines) - FIXME marked RESOLVED Commits: - `0239cc1` - Add test suite for invalid parent assignment bugs - `899fa3b` - Add config validation for parent-child distances - `4d10be1` - Update documentation with resolution status - <current commit> - Add session summary	6 months ago
cinnaboot	748a309995	Move implementation session summary to session summaries - Extract Implementation Session Summary from mission_planning.md - Create new session summary: 2026-01-18-mission-planning-leo-impulse-burn.md - Keep Current Issue Identified section in mission_planning.md - Session summary includes: Phases 0-4 work, test results, delta-v bug analysis, next steps	6 months ago
cinnaboot	a6a8a34a6e	add session summary	6 months ago
cinnaboot	91636d990f	Add session summary for body selection UI implementation Comprehensive documentation of: - Raygui integration and UI panel implementation - Camera follow feature with orbital mechanics - Bug fixes (GuiListView, buffer safety, orbit rotation) - Distance preservation when switching bodies - User experience improvements (removed keyboard shortcuts) - Technical details and implementation notes Summary covers all 12 commits in feature/body-selection-ui branch.	6 months ago
cinnaboot	eb54728123	Update implementation plans for completed UI feature - Mark all UI implementation phases as completed in ui_implementation_plan.md - Add UI body selection to completed items in implementation_plan.md - Move ui_implementation_summary.md to docs/session_summaries/ for better organization	6 months ago
cinnaboot	49fc735717	add session summary	6 months ago
cinnaboot	0722ca7114	Add session summary for parabolic/hyperbolic testing Document comprehensive testing of three orbit types: - Parabolic orbit support (e=1.0) with escape velocity formula - Hyperbolic orbit testing (e>1.0) with asymptotic velocity - Simplified SOI transition test (3-body system) - Hysteresis creates one-way SOI barrier - 39 new assertions across 8 test cases - Net +364 lines across 10 files Claude	6 months ago
cinnaboot	5526fdf84e	add llm session summary	6 months ago
cinnaboot	8ca1bd8042	Add session summary for hierarchical coordinate frames implementation Comprehensive summary of Phase 1-2 implementation: - Multiple root bodies cleanup (-154 lines) - Phase 1: Dual coordinate storage foundation - Phase 2: Local frame integration (Earth Moon test passing!) - Test improvements: 6/9 → 7/9 passing - Technical details and architecture documentation - Future work and deferred phases noted	6 months ago
cinnaboot	756a3b9566	add session summary	6 months ago
cinnaboot	81e799c2ec	Rename bodies.h/cpp to simulation.h/cpp - Renamed src/bodies.h to src/simulation.h - Renamed src/bodies.cpp to src/simulation.cpp - Updated all include references in src/ and tests/ - Updated Makefile to reference simulation.cpp - Updated documentation references Claude	6 months ago
cinnaboot	fd8a62de4b	add session summary	6 months ago
cinnaboot	088a1dac62	add session summary	6 months ago
cinnaboot	c4cf32a878	Add session summary for 2026-01-05	6 months ago
cinnaboot	a8457479d6	add session summary from yesterday	6 months ago
cinnaboot	b3c2fa4c91	add session summary format 🤖 Generated with [Claude Code](https://claude.com/claude-code) Co-Authored-By: Claude Sonnet 4.5 <noreply@anthropic.com>	6 months ago
cinnaboot	5d34eef4d0	move docs/sessions to docs/session_summaries	6 months ago

25 Commits (2b68e2e579d3bbecee1daaf92dce7e9301ed606c)