MagneticUnloadingDemo:

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

Children:

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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