Tags: JuliaSpace/SatelliteToolbox.jl
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[Diff since v0.10.0](v0.10.0...v0.10.1) The package now supports the new format of the EOP files finals.all.csv and finals2000A.all.csv introduced in November 6, 2023.] **Merged pull requests:** - Clear confusion about geomagnetic field vector (#85) (@yakir12) - :docfix: Renamed r_ecef_to_eci in doc text to r_eci_to_eci. (#88) (@srikumarks) - Remove unused type variable (#90) (@yakir12) - 📚 Add the code to create the Celestrak TLE fetcher (#99) (@yanma) **Closed issues:** - Consider breaking out components? (#1) - Add documentation for API functions that converts state vectors (#26) - Increase precision in ref. system conversions (#64) - Automatically download TLE (#70) - Docstring update for getters functions (#73) - IERS data service down (#78) - Allow the propagators to initialize the structure in place (#86) - 2023 Space Index File not available (#87) - Discrepancies between J2 Propagator and STK J2Perturbations (#91) - sgp4 propagator accuracy (#92) - ITRF to TEME transformation (#93) - Can't find ground_station_accesses in v0.10.0 (#94) - init_orbit_propagator method definition warning (#96) - Add `geocentric_to_ecef`? (#98)
[Diff since v0.9.4](v0.9.4...v0.9.5) - The package now supports the new format of the EOP files `finals.all.csv` and `finals2000A.all.csv` introduced in November 6, 2023. **Merged pull requests:** - Remove @eval from @RemoteFile macro call (#76) (@disberd) - Fix documentation typos (#77) (@yashi) - 📚 Fix typo for the altitude of geocentric_to_geodetic() (#79) (@yashi) - Bump Interpolations to v0.14 (#82) (@fgasdia) - CompatHelper: bump compat for PrettyTables to 2, (keep existing compat) (#83) (@github-actions[bot]) - CompatHelper: bump compat for RemoteFiles to 0.5, (keep existing compat) (#84) (@github-actions[bot]) - Clear confusion about geomagnetic field vector (#85) (@yakir12) - :docfix: Renamed r_ecef_to_eci in doc text to r_eci_to_eci. (#88) (@srikumarks) - Remove unused type variable (#90) (@yakir12) - 📚 Add the code to create the Celestrak TLE fetcher (#99) (@yanma) **Closed issues:** - Consider breaking out components? (#1) - Add documentation for API functions that converts state vectors (#26) - Increase precision in ref. system conversions (#64) - Automatically download TLE (#70) - Docstring update for getters functions (#73) - Precompilation error when SatelliteToolbox and get_iers_eop are used as dependencies (#75) - IERS data service down (#78) - Daily Ap index using get_Ap() and get_space_indices() (#80) - Allow the propagators to initialize the structure in place (#86) - 2023 Space Index File not available (#87) - Discrepancies between J2 Propagator and STK J2Perturbations (#91) - sgp4 propagator accuracy (#92) - ITRF to TEME transformation (#93) - Can't find ground_station_accesses in v0.10.0 (#94) - init_orbit_propagator method definition warning (#96) - Add `geocentric_to_ecef`? (#98)
[Diff since v0.10.0](v0.10.0...v0.11.0) **Closed issues:** - Consider breaking out components? (#1) - Add documentation for API functions that converts state vectors (#26) - Increase precision in ref. system conversions (#64) - Automatically download TLE (#70) - Docstring update for getters functions (#73) - IERS data service down (#78) - Allow the propagators to initialize the structure in place (#86) - 2023 Space Index File not available (#87) - Discrepancies between J2 Propagator and STK J2Perturbations (#91) - sgp4 propagator accuracy (#92) - ITRF to TEME transformation (#93) - Can't find ground_station_accesses in v0.10.0 (#94) - init_orbit_propagator method definition warning (#96) **Merged pull requests:** - Clear confusion about geomagnetic field vector (#85) (@yakir12) - :docfix: Renamed r_ecef_to_eci in doc text to r_eci_to_eci. (#88) (@srikumarks) - Remove unused type variable (#90) (@yakir12)
[Diff since v0.9.4](v0.9.4...v0.10.0) - The support for Julia 1.0 was dropped. - The function `satellite_position_i` was removed. - All the functions with analysis were removed because they will be implemented in [SatelliteAnalysis.jl](https://github.com/JuliaSpace/SatelliteAnalysis.jl). - The keyword argument `vJD` was renamed to `vjd` in `rv_to_mean_elements_sgp4`. - The keyword argument `max_it` was renamed to `max_iterations` in `rv_to_mean_elements_sgp4`. - The function `compute_RAAN_lt` was renamed to `ltan_to_raan`. - The epoch was not being correctly obtained by `get_epoch` in the J2 osculating propagator. - The maximum degree used when computing the IGRF can now be selected using the keyword argument `max_degree`. - Many functions now supports other type of floats, including the orbit propagators. - The keyword argument `print_debug` was added to `rv_to_mean_elements_sgp4` to print debugging information. - The function `data_to_jd` now supports milliseconds. (PR #71) - The EOP remote files are now updated every week. - Many performance improvements in the functions. **Closed issues:** - Precompilation error when SatelliteToolbox and get_iers_eop are used as dependencies (#75) - Daily Ap index using get_Ap() and get_space_indices() (#80) **Merged pull requests:** - Remove @eval from @RemoteFile macro call (#76) (@disberd) - Fix documentation typos (#77) (@yashi) - 📚 Fix typo for the altitude of geocentric_to_geodetic() (#79) (@yashi) - Bump Interpolations to v0.14 (#82) (@fgasdia) - CompatHelper: bump compat for PrettyTables to 2, (keep existing compat) (#83) (@github-actions[bot]) - CompatHelper: bump compat for RemoteFiles to 0.5, (keep existing compat) (#84) (@github-actions[bot])
[Diff since v0.9.3](v0.9.3...v0.9.4) - The conversion from RV to Keplerian elements had a bug for Equatorial and elliptical orbits. (Issue #72) **Closed issues:** - Fix documentation in nutation_fk5 (#62) - Remove unused variables (#63) - Why the track is not drifting? (#65) - Reference to geodesic coordinate frames (#66) - Wrong docstring for rv_to_mean_elements_j2osc (#67) - Quick fix to rv_to_kepler (#72) **Merged pull requests:** - Clerical error (#68) (@tony1980) - Added milliseconds to date_to_jd(::DateTime). (#71) (@justbyoo)
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