Path: SC/Attitude
% Right-hand-side for attitude dynamics with a permanent magent -------------------------------------------------------------------------- Form: [xDot,torque,bFBody] = PermanentMagnetRHS( x, t, d ) -------------------------------------------------------------------------- ------ Inputs ------ x (7,1) State vector [qEB; wB] t (1,1) Time (seconds from Julian date epoch d.jD0) d (.) Data structure with jD0, inertia, mu, t, r ------- Outputs ------- xDot (7,1) State derivatives torque (3,1) Torque applied bFBody (3,1) Earth magnetic field in body frame --------------------------------------------------------------------------
AerospaceUtils: Coord/QIToBDot Orbit: OrbitMechanics/RVOrbGen SC: Disturbances/GravityGradientFromR SC: Environs/BDipole Common: Quaternion/QForm Common: Time/Date2JD Math: Linear/Cross
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