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2 Commits (ee055856a5b47851ed9ac731c5edb8ce76be3386)

Author	SHA1	Message	Date
cinnaboot	ee055856a5	fix: enable SOI exit transitions with conditional hysteresis ... Modified find_dominant_body() to detect when bodies exit SOI by checking distance against current parent's SOI radius. Applies different hysteresis: - Inside SOI: 0.5x distance threshold prevents oscillations - Outside SOI: switches to closest body without hysteresis Added test requirement for Mars SOI exit detection. Claude	6 months ago
cinnaboot	08cdfeb7ca	Add simplified SOI transition test case ... - Create soi_transition.toml with Sun + Mars + SmallBody (3 bodies) - Add test_soi_transition.cpp with 2 test cases: * SOI transition from Sun to Mars (validates one-way transition) * SOI radii calculation verification - Use comet parameters (e=0.7, a=3.74e11) for Mars encounter - Document hysteresis makes Mars -> Sun exit impossible - Simpler than original 7-body test_comet_orbit.cpp - All 3 SOI tests pass (12 assertions total) Claude	6 months ago