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This becomes important when we wish the attitude (one of the axis) of the spacecraft to align to the spacecraft ground-track, which in turn requires one of the axis of the spacecraft body to be aligned to the spacecraft velocity in Earth-Fixed frame.
The text was updated successfully, but these errors were encountered:
vinay0000
changed the title
GMAT-OC ECI to EarthFixed rotation matrix is computed ignoring Earth's rotation term
propcov-cpp ECI to EarthFixed rotation matrix is computed ignoring Earth's rotation term
Jan 14, 2022
vinay0000
changed the title
propcov-cpp ECI to EarthFixed rotation matrix is computed ignoring Earth's rotation term
propcov-cpp ECI to EarthFixed conversion is computed ignoring Earth's rotation term
May 31, 2022
Corresponding function:
CoverageChecker::GetEarthFixedSatState(Real jd, const Rvector6& scCartState)
This becomes important when we wish the attitude (one of the axis) of the spacecraft to align to the spacecraft ground-track, which in turn requires one of the axis of the spacecraft body to be aligned to the spacecraft velocity in Earth-Fixed frame.
The text was updated successfully, but these errors were encountered: