Ryan Malloy
6e57071970
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.
31 lines
312 B
Plaintext
31 lines
312 B
Plaintext
# Build artifacts
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*.o
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*.bc
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*.so
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*.dylib
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# pg_regress output
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regression.diffs
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regression.out
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results/
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tmp_check/
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log/
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# Editor files
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*.swp
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*.swo
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*~
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.vscode/
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.idea/
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# Test artifacts
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test/matrix-logs/
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test/test_de_reader
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test/test_od_math
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test/test_od_iod
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# Docs site
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docs/node_modules/
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docs/dist/
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docs/.astro/
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