Path: FormationFlying/Transformation
% Compute element differences from Hills frame state and ref. elements
Since version 7.
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Inputs
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el0 (1,6) reference orbital elements
xH (6,:) relative position and velocity in Hills frame [km; km/s]
type (1) type of orbital element set
1 -- [a,th,i,q1,q2,W]
2 -- [a,i,W,w,e,M]
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Outputs
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dEl (:,6) Orbital Element differences
if type 1 -- delta [a,th,i,q1,q2,W]
if type 2 -- delta [a,i,W,w,e,M]
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FormationFlying: Coord/GetHillsMats FormationFlying: Transformation/Hills2ECI Orbit: OrbitCoord/Alfriend2El Orbit: OrbitCoord/El2Alfriend Orbit: OrbitCoord/OrbElemDiff SC: BasicOrbit/CP2I SC: BasicOrbit/E2M SC: BasicOrbit/E2Nu SC: BasicOrbit/El2RV SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/M2Nu SC: BasicOrbit/M2NuPb SC: BasicOrbit/Nu2E SC: BasicOrbit/Nu2M SC: BasicOrbit/RV2El Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/DispWithTitle Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Math: Linear/Cross Math: Linear/Dot Math: Linear/DupVect Math: Linear/Mag Math: Trigonometry/WrapPhase
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