Research Article
Active Disturbance Rejection Attitude Control for Hypersonic Vehicle Based on Intelligent Stochastic Robust Optimization Method
Figure 7
Steering curves of the servo in the four cases: (a) rudder deflection with baseline without uncertainties, (b) rudder deflection with baseline under uncertainties, (c) rudder deflection with optimal parameters without uncertainties, and (d) rudder deflection with optimal parameters under uncertainties.
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(b) |
(c) |
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