|
SUPPORT SITE |
|
|
|
SUPPORT SITE |
|
Path: SCPro/DynamicalModels
% Right-hand-side of the spacecraft dynamical equations.
This function includes position, orientation
and 4 reaction wheels. It also includes time varying inertia.
This simulation is primarily to analyze control during deployment.
Several f
--------------------------------------------------------------------------
-------
Inputs
-------
x (:,1) State vector
t ( 1,1) Time
sim ( 1,1) Data structure for the simulation
.uRWA (3,4) Reaction wheel unit vectors
.tRWA (4,1) Reaction wheel torque
.funIandD (1,:) Disturbance and inertia model
.tExt (3,1) Other external torques
-------
Outputs
-------
xDot (:,1) State vector derivative
--------------------------------------------------------------------------
AerospaceUtils: Coord/QIToBDot Math: Linear/Cross SC: BasicOrbit/FOrbCart
Back to the SCPro Module page