|
SUPPORT SITE |
|
|
|
SUPPORT SITE |
|
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 --------------------------------------------------------------------------
AeroUtils: Coord/QIToBDot Common: Quaternion/QForm Math: Linear/Cross SC: Disturbances/GravityGradientFromR SC: Environs/BDipole
Back to the SC Module page