Path: FormationFlying/Coord
% Calculates orbital elements for an in-line formation. -------------------------------------------------------------------------- Form: elSet = ProjLine( aRef, iRef, kSats, rF ) -------------------------------------------------------------------------- ------ Inputs ------ aRef (1,1) Semi-major axis of reference orbit [km] iRef (1,1) Inclination of reference orbit [rad] kSats (1,1) Number of satellites rF (1,1) Distance between satellites [km] ------- Outputs ------- elSet (kSats,6) Orbital elements of all spacecraft rH (3,kSats) Radius vector in Hills frame [km] vH (3,kSats) Velocity vector in Hills frame [km/s] --------------------------------------------------------------------------
FormationFlying: Coord/GetHillsMats FormationFlying: Transformation/ECI2Hills 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
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