Path: SC/Dynamics
% Rigid body right-hand-side with magnetic torque computed internally.
Models a point-mass orbit.
This function is called by RK4. See also MagneticControlSim.
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Form:
xDot = FRBWithMag( x, t, d )
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Inputs
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x (13,1) The state vector [r;v;q;w]
t Time
d (.) Data structure
.mu (1,1) Gravitational parameter
.inr (3,3) Inertia
.invInr (3,3) Inverse inertia
.tExt (3,1) External torque
.bECI (3,1) Magnetic field in ECI frame
.dipole (3,1) Magnetic dipole in spacecraft frame
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Outputs
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xDot (13,1) The derivative of the state vector
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AC: ACData/ACTConstants AerospaceUtils: Coord/QIToBDot SC: Dynamics/RBModel SC: SCData/sCTConstants Common: CommonData/Constants Common: CommonData/xSplashSmall Common: Control/C2DZOH Common: Database/Constant Common: General/DeleteCell Common: Quaternion/QForm Math: Linear/Cross Math: Linear/Mag Math: Linear/SkewSymm
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