ADUKF2SensorSim:

% 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.

  Since version 8.
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  See also AttDetUKF, ADUKFSensorSim, StarSensor, RIGOut, Q2Mat, QMult, 
  QPose, QUnit, Plot2D, RK4, IntGyroQuaternion, RandSC, UKUDF
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%
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   Copyright (c) 1994, 2008, 2009 Princeton Satellite Systems, Inc.
   All rights reserved.
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Children:

Common: Estimation/UKF
Common: Estimation/UKUDF
Common: Graphics/Plot2D
Common: Quaternion/Q2Mat
Common: Quaternion/QMult
Common: Quaternion/QPose
Common: Quaternion/QUnit
Math: Integration/RK4
SC: Sensor/RIGOut
SpacecraftEstimation: StellarAttDet/AttDetUKF
SpacecraftEstimation: StellarAttDet/IntGyroQuaternion
SpacecraftEstimation: StellarCatalog/RandSC
SpacecraftEstimation: StellarModels/FRBwRIG
SpacecraftEstimation: StellarModels/StarSensor