Tree: e41185c4be

main

test-refactor

Branches Tags

${ item.name }

Create tag ${ searchTerm }

Create branch ${ searchTerm }

from 'e41185c4be'

${ noResults }

Commit Graph

3 Commits (e41185c4be1d993645c597ffdb8604c2f6f9e768)

Author	SHA1	Message	Date
cinnaboot	161198d9db	Update planning doc and add session summary for Molniya orbit implementation	5 months ago
cinnaboot	b221251787	Remove altitude parameter to fix spacecraft initialization bug ... - Remove altitude convenience parameter from body and spacecraft config parsing - Update test configs to use explicit semi_major_axis instead of altitude - Remove buggy post-processing loop that added parent radius to all spacecraft - Result: Semi-major axis now used as-is (correct behavior) - Test results: Molniya position tests now pass (was failing by 1-11M meters) - Documentation: Remove altitude references from technical reference - Planning: Document bug fix decision and implementation details Changes: - src/config_loader.cpp: Remove altitude parsing and post-processing - tests/test_maneuver_planning.toml: Use semi_major_axis = 6.771e6 - tests/test_maneuvers.toml: Use semi_major_axis = 6.771e6 - tests/test_orbit_rendering.toml: Use semi_major_axis = 6.771e6 - docs/technical_reference.md: Remove altitude documentation - docs/planning/molniya-orbit-test-plan.md: Document bug fix approach	5 months ago
cinnaboot	cfb2c92bd4	Add Molniya orbit test cases and document config loader bug ... - Create test configuration for Molniya orbits with Earth as root body - Implement test suite for highly inclined orbits: * Position verification at multiple true anomalies * Orbital period verification * Generic inclined orbit test * Inclination parameter preservation - Document critical bug in spacecraft initialization: * Config loader incorrectly adds parent radius to semi_major_axis * Affects all spacecraft using semi_major_axis directly * Causes significant position errors (1-11M meters) * Molniya tests fail due to this bug, not test code	5 months ago