MomentumManagement:

Path: CubeSat/Demos/Simulation

% Demonstrate simple dipole based momentum management
   This uses a pseudo-inverse to get the best fit between the available
   dipoles and the desired momentum unloading torque.

   Since version 9.
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  See also Plot2D, TimeLabl, RK4, Date2JD, MomentumUnloading, 
  RHSMomentum, Period, BDipole
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%
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   Copyright (c) 2010 Princeton Satellite Systems, Inc.
   All rights reserved.
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Children:

Common: Graphics/Plot2D
Common: Graphics/TimeLabl
Common: Time/Date2JD
CubeSat: AttitudeControl/MomentumUnloading
CubeSat: Simulation/RHSMomentum
Math: Integration/RK4
SC: BasicOrbit/Period
SC: Environs/BDipole

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