收稿日期: 2017-05-25
修回日期: 2017-06-27
网络出版日期: 2017-06-27
基金资助
国家自然科学基金（60674090）
Design of carrier UAV lateral/directional landing control law
Received date: 2017-05-25
Revised date: 2017-06-27
Online published: 2017-06-27
Supported by
National Natural Science Foundation of China (60674090)
张杨 , 吴文海 , 汪杰 . 舰载无人机横侧向着舰控制律设计[J]. 航空学报, 2017 , 38(S1) : 721489 -721489 . DOI: 10.7527/S1000-6893.2017.721489
Carrier UAV lateral/directional landing has been one of the difficulties in control design. To solve this problem, the nonlinear model for the carrier UAV is solved by the backstepping method. To solve the ‘problem of expansion’ of traditional backstepping method, the command filtered method is introduced, and only one Lyapunov function is designed to prove the stability. In addition, for the carrier UAV model can not be obtained accurately, the adaptive method is adopted to estimate it. The designed controller can better solve the coupling problem in lateral/directional control. A comparison with the traditional PID simulation shows that the control law in this paper can meet the requirements for the performance of reference signal tracking.
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