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. ---------------------------------------------------------------------- See also Plot2D, TimeLabl, RK4, Date2JD, MomentumUnloading, RHSMomentum, Period, BDipole ------------------------------------------------------------------------ % ------------------------------------------------------------------------ Copyright (c) 2010 Princeton Satellite Systems, Inc. All rights reserved. ------------------------------------------------------------------------
Common: Graphics/Plot2D Common: Graphics/TimeLabl Common: Time/Date2JD CubeSat: AttitudeControl/MomentumUnloading CubeSat: Simulation/RHSMomentum Math: Integration/RK4 SC: BasicOrbit/Period SC: Environs/BDipole
Back to the CubeSat Module page