ADUKF2SensorSim:

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   Test a star sensor attitude determination system with gyros.
   This system has two sensors and also estimates the angle between
   the sensors.

   This can use the unscented Kalman Filter (UKF) or the EKF.
   dT is the time step for the attitude determination system. You can 
   numerically integrate with a smaller time step by setting nInt > 1.

   See also AttDetUKF, ADUKFSensorSim, StarSens, RIGOut.
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Children:

Common: Coord/Q2Mat
Common: Coord/QMult
Common: Coord/QPose
Common: Coord/QUnit
Common: Graphics/Plot2D
Common: Math/RK4
Estimation: StellarAttDet/AttDetUKF
Estimation: StellarAttDet/IntGyroQuaternion
Estimation: StellarCatalog/RandSC
Estimation: StellarModels/StarSens
Estimation: UKF/UKF
Estimation: UKF/UKUDF
SC: Sensor/RIGOut