Path: FormationFlying/Control
% Relative orbit control using LQG Note: This demo requies the Mu-Analysis and Synthesis Toolbox. ------------------------------------------------------------------------ See also AC, QCE, QCR, LinOrbLQG, DiscreteHills, LPCircular, LinOrb, OrbRate, Period ------------------------------------------------------------------------ % ------------------------------------------------------------------------- Copyright (c) 2004 Princeton Satellite Systems, Inc. All rights reserved. Since version 7. ------------------------------------------------------------------------- 24-Feb-2017: Update output from LinOrbLQG (4 matrices) -------------------------------------------------------------------------
FormationFlying: Control/LinOrbLQG FormationFlying: Dynamics/DiscreteHills FormationFlying: EccDynamics/FFEccLinOrb FormationFlying: LP/LPCircular FormationFlying: Utility/NuDot Orbit: RHSOrbit/LinOrb SC: BasicOrbit/E2Nu SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/M2Nu SC: BasicOrbit/M2NuPb SC: BasicOrbit/OrbRate SC: BasicOrbit/Period Common: CommonData/SwooshWatermark Common: Control/C2DZOH Common: Control/QCE Common: Control/QCR Common: Control/Riccati Common: General/CellToMat Common: General/DispWithTitle Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Math: Analysis/Simplex Math: Analysis/Simplex2 Math: Linear/DupVect Math: Linear/InvP Math: Linear/Mag Math: MathUtils/Odd
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