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

Figure 4

Histories of mean values of the four estimated aerodynamic derivatives in Monte Carlo simulation. The means with 95% bands for every step are fitted by the normal distribution and compared with the reference values: (a) statistics of ; (b) statistics of ; (c) statistics of ; (d) statistics of .

(a)

(b)

(c)

(d)