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pg_orrery/test
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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
..
data
Vendor SGP4/SDP4 as pure C, drop g++ dependency
2026-02-17 12:45:39 -07:00
expected
Add Gibbs IOD bootstrap for seed-free orbit determination
2026-02-17 16:06:05 -07:00
sql
Add Gibbs IOD bootstrap for seed-free orbit determination
2026-02-17 16:06:05 -07:00
pg-version-matrix.sh
Add PG version test matrix (14-18)
2026-02-17 14:53:32 -07:00
test_de_reader.c
Rename pg_orbit to pg_orrery
2026-02-17 13:36:22 -07:00
test_od_iod.c
Add Gibbs IOD bootstrap for seed-free orbit determination
2026-02-17 16:06:05 -07:00
test_od_math.c
Add observation-to-TLE fitting (orbit determination) for v0.4.0
2026-02-17 15:44:48 -07:00