Path: FormationFlying/Initialize
% Attitude control test data structure Set up the data structure for a DFF simulation which tests the functionality of the attitude control system. All inputs are optional. -------------------------------------------------------------------------- Form: sim = TestADCSSimStruct( el, nOrbits, nSC, jD ) -------------------------------------------------------------------------- ------ Inputs ------ el (n,:) Initial element set for all spacecraft. duration (1) Simulation duration (sec). nSC (1) Number of spacecraft to simulate. jD (1) Julian date at start of simulation. ------- Outputs ------- sim (.) Simulation data structure to be input to DFFSimulation --------------------------------------------------------------------------
FormationFlying: Coord/CirclePhase FormationFlying: Coord/InitializeFormation FormationFlying: DataStructures/Geometry_Structure FormationFlying: Transformation/DeltaElem2Hills FormationFlying: Transformation/Goals2Hills FormationFlying: Transformation/Hills2DeltaElem 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/OrbRate Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/DispWithTitle Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Time/DTSToDTA Common: Time/Date2JD Common: Time/JD2000 Math: Linear/DupVect Math: Trigonometry/WrapPhase
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