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% Momentum unloading with magnetic torque Perform a long-term simulation of just the momentum unloading using magnetic torque. Performs Euler integration of the momentum vector in the ECI frame. This shows how the 3 axis torque is met over the course of the orbit depsite the mismatch at each time step. See also MomentumUnloading, PlotOrbit, Period, RVOrbGen, BDipole, Figui, TimeHistory, Date2JD, Skew
CubeSat: AttitudeControl/MomentumUnloading CubeSat: Visualization/PlotOrbit Orbit: OrbitMechanics/Period Orbit: OrbitSim/RVOrbGen SC: Environs/BDipole Common: GUIs/Figui Common: Graphics/TimeHistory Common: Time/Date2JD
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