Active Disturbance Rejection Attitude Control for Hypersonic Vehicle Based on Intelligent Stochastic Robust Optimization Method

Figure 6

Angular velocity curves in the four cases: (a) angular velocity curve with baseline without uncertainties, (b) angular velocity curve with baseline under uncertainties, (c) angular velocity curve with optimal parameters without uncertainties, and (d) angular velocity curve with optimal parameters under uncertainties.

(a)

(b)

(c)

(d)