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pg_orrery/test/expected
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Ryan Malloy 6e57071970 Add Gibbs IOD bootstrap for seed-free orbit determination 
Eliminates the seed TLE requirement for topocentric fitting by
computing an initial orbit estimate from 3 well-spaced observations
using the Gibbs method. ECI fitting retains the single-observation
r,v approach (exact for two-body) with Gibbs as fallback.
2026-02-17 16:06:05 -07:00
..
convenience.out
Rename pg_orbit to pg_orrery
2026-02-17 13:36:22 -07:00
coord_transforms.out
Rename pg_orbit to pg_orrery
2026-02-17 13:36:22 -07:00
de_ephemeris.out
Rename pg_orbit to pg_orrery
2026-02-17 13:36:22 -07:00
gist_index.out
Rename pg_orbit to pg_orrery
2026-02-17 13:36:22 -07:00
kepler_comet.out
pg_orbit 0.2.0: Full solar system computation at the SQL layer
2026-02-16 01:36:27 -07:00
lambert_transfer.out
Add PG version test matrix (14-18)
2026-02-17 14:53:32 -07:00
moon_observe.out
Phase 3: Planetary moons and Jupiter radio burst prediction
2026-02-16 01:55:13 -07:00
od_fit.out
Add Gibbs IOD bootstrap for seed-free orbit determination
2026-02-17 16:06:05 -07:00
pass_prediction.out
Rename pg_orbit to pg_orrery
2026-02-17 13:36:22 -07:00
planet_observe.out
pg_orbit 0.2.0: Full solar system computation at the SQL layer
2026-02-16 01:36:27 -07:00
sgp4_propagate.out
Rename pg_orbit to pg_orrery
2026-02-17 13:36:22 -07:00
star_observe.out
pg_orbit 0.2.0: Full solar system computation at the SQL layer
2026-02-16 01:36:27 -07:00
tle_parse.out
Rename pg_orbit to pg_orrery
2026-02-17 13:36:22 -07:00
vallado_518.out
Rename pg_orbit to pg_orrery
2026-02-17 13:36:22 -07:00