MagneticControlDemo:

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.

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   Copyright (c) 2011-2012 Princeton Satellite Systems, Inc.
   All rights reserved.
   Since version 10.
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Children:

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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