The control law is based on the nonlinear dynamic inversion, and the neural network is used to cancel the inversion error induced by aircraft actuator Failures. 本文以非線(xiàn)性動(dòng)態(tài)逆方法為基本控制律，通過(guò)設計的自適應神經(jīng)網(wǎng)絡(luò )，實(shí)時(shí)補償因操縱面故障而引起的逆誤差。
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