Path: Missions/SpaceStation
% 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