Path: SC/DemoFuns
% Dynamics of spacecraft with one reaction wheel. Used by FMagSim2 and FMagSimWithEstimator. -------------------------------------------------------------------------- Form: xDot = FMagSim( x, t, inr, invInr, tExt, inrW, uW, tW, eSAC ) -------------------------------------------------------------------------- ------ Inputs ------ x (8,1) The state vector t (1,1) Time (unused) inr (3,3) Inertia invInr (3,3) Inverse inertia tExt (3,1) External torque inrW (1,1) RWA inertia uW (3,1) RWA unit vector tW (1,1) RWA torque ------- Outputs ------- xDot (15,1) The derivative of the state vector See also QIToBDot, GSModel --------------------------------------------------------------------------
AerospaceUtils: Coord/QIToBDot SC: Dynamics/GSModel Common: Control/C2DZOH Math: Linear/Cross Math: Linear/SkewSymm
Back to the SC Module page