Path: CubeSat/Simulation
% Demonstrate simple dipole based momentum management
This uses projection to get the best fit between the available
dipoles and the desired momentum unloading torque.
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See also Plot2D, TimeLabl, RK4, Date2JD, MomentumUnloading,
RHSMomentum, Period, BDipole
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Copyright (c) 2010, 2021 Princeton Satellite Systems, Inc.
All rights reserved.
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Since version 9.
2021.2 Now uses the torque from the torquers in the inertial frames.
Now uses TimeHistory, instead of Plot2D
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CubeSat: AttitudeControl/MomentumUnloading Orbit: OrbitMechanics/RVOrbGen SC: Environs/BDipole Common: Graphics/TimeHistory Common: Time/Date2JD Math: Integration/RK4
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