RHSSpacecraftWithIMU:

Path: SCPro/DynamicalModels

%  Right-hand-side for a spacecraft with an IMU 
 Right hand side for a spacecraft with an inertial measurement unit.
 The spacecraft is a rigid body orbiting around a point mass. 

 d = RHSSpacecraftWithIMU

 returns the default data structure. Uses the IMU function.

--------------------------------------------------------------------------
   Form:
   xDot = RHSSpacecraftWithIMU( x, ~, d )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   x           (19,1)   [r;v;q;omega;randomWalk]
   t           (1,1)    Time (unused)
   d           (.)      Data structure
                        .inr         (3,3) Inertia matrix (kg-m^2)
                        .torque      (3,1) Torque (Nm)
                        .accel       (3,1) Acceleration ECI (km/s^2)
                        .mu          (1,1) Gravity constant (km^3/s^2)
                        .iMU       	(.)   See IMU
   -------
   Outputs
   -------
   x           (19,1)   d[r;v;q;omega;randomWalk]/dt

--------------------------------------------------------------------------

Children:

AerospaceUtils: Coord/QIToBDot
SCPro: ProSensors/IMU
Common: Control/C2DZOH
Common: Quaternion/QForm
Math: Linear/Cross
Math: Linear/Mag
Math: Linear/Skew
Math: Linear/SkewSq
Math: Linear/SkewSymm

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