Path: FormationFlying/Control
% Demonstrates control of a large formation of satellites. LargeFormationControl computes the control for a large formation. Control is respect to the origin LargeFormationControt for a demo. -------------------------------------------------------------------------- Form: [x,a] = LargeFormationControl( x0, d ) -------------------------------------------------------------------------- ------ Inputs ------ r (6,1) Initial state of the center d (.) Input data structure ------- Outputs ------- xP (6*n,:) States for each spacecraft aP (3*n,:) Acceleration each spacecraft t (1,:) Corresponding times (s) --------------------------------------------------------------------------
Orbit: OrbitMechanics/APlanet SC: BasicOrbit/CP2I 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/Period SC: Ephem/MoonV1 SC: Ephem/RMoonECI SC: Ephem/RSunECI SC: Ephem/SunV1 Common: CommonData/SwooshWatermark Common: GUIs/TimeDisplay Common: General/CellToMat Common: General/DispWithTitle Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/TimeLabl Common: Time/DTSToDTA Common: Time/Date2JD Common: Time/JD2000 Math: Integration/RK4 Math: Linear/DupVect Math: Linear/Mag Math: Linear/Unit Math: Trigonometry/CosD Math: Trigonometry/SinD
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