A Bayesian Adaptive Unscented Kalman Filter for Aircraft Parameter and Noise Estimation

Figure 2

Comparison of the system measurement data with the estimated states. The data is estimated by the Bayesian UKF algorithm, and the system inputs are given in the last figure: (a) velocity comparison; (b) angle of attack comparison; (c) pitch rate comparison; (d) angle of pitch comparison; (e) height comparison; (f) system input.

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