UnscentedKalmanSmootherDemo:

Path: SpacecraftEstimation/Demos/OrbitEstimation

% UKF/UKS demonstration.

   This is for a 1 dimensional launch problem with an angle sensor that 
   measures the angle to the launch vehicle. The vehicle is subject
   to Gaussian random thrust variations. The sensor is subject to Gaussian
   white noise.

   The script first runs the simulation and the sensor angle are used
   for both the forward and backward Unscented Kalman filters.

   The geometry gets worse as the launch vehicle gets higher.

   The demo uses UKFUpdate and UKFPredict which are alternatives to UKF.

   Since version 11.
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  See also RHSX, AngleSensor, KFInitialize, UKFWeight, UKFPredict,
  UKFUpdate, KalmanFilterCombine
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%
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   Copyright (c) 2012 Princeton Satellite Systems, Inc.
   All rights reserved.
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Children:

Common: Estimation/AngleSensor
Common: Estimation/KFInitialize
Common: Estimation/KalmanFilterCombine
Common: Estimation/RHSX
Common: Estimation/UKFPredict
Common: Estimation/UKFUpdate
Common: Estimation/UKFWeight
Common: Graphics/Plot2D
Common: Graphics/TimeLabl
Math: Integration/RK4

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