Lucy e2c706ecb0 Fix: recompute sun-frame trail and SOI crossings after flyby ...

After SOI exit the asteroid has new orbital elements (gravity assist).
Previously the old trail and crossing predictions were never updated,
causing three bugs:
  1. Old trajectory still drawn after exit
  2. Next SOI entry time based on stale orbit
  3. Subsequent SOI entries never triggered

Now on exit: recompute trail, rescans for future SOI crossings,
and resets the crossing index.

2026-05-21 20:35:17 +02:00

frame_transition.py

Initial commit: Keplerian orbital mechanics with patched-conics SOI transitions

2026-05-21 20:31:17 +02:00

orbit_drawer.py

Initial commit: Keplerian orbital mechanics with patched-conics SOI transitions

2026-05-21 20:31:17 +02:00

orbital_elements.py

Initial commit: Keplerian orbital mechanics with patched-conics SOI transitions

2026-05-21 20:31:17 +02:00

soi_calculator.py

Initial commit: Keplerian orbital mechanics with patched-conics SOI transitions

2026-05-21 20:31:17 +02:00

test_orbital.py

Initial commit: Keplerian orbital mechanics with patched-conics SOI transitions

2026-05-21 20:31:17 +02:00

visual_test.py

Fix: recompute sun-frame trail and SOI crossings after flyby

2026-05-21 20:35:17 +02:00

Description

Keplerian orbital mechanics test suite with patched-conics SOI transitions

49 KiB

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