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Path: CubeSat/Demos/AttitudeControl
% Magnetic control demand analysis Put a satellite aligned with LVLH (nadir-pointing) in a 350 km inclined orbit and evaluate the ability of the magnetic control to create a particular torque along the orbit. There are 3 orthogonal torquers. Note that the pure x torque can only be created at certain points along the orbit. ------------------------------------------------------------------------- % -------------------------------------------------------------------------- Copyright (c) 2011-2012 Princeton Satellite Systems, Inc. All rights reserved. Since version 10. --------------------------------------------------------------------------
AerospaceUtils: Coord/QLVLH Common: Graphics/Plot2D Common: Graphics/TimeLabl Common: Quaternion/QForm Common: Time/Date2JD CubeSat: AttitudeControl/MagneticControl CubeSat: Visualization/PlotOrbit Math: Linear/Cross Math: Linear/Mag SC: BasicOrbit/RVFromKepler SC: Environs/BDipole
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