Design of carrier landing controller based on adaptive dynamic inversion

被引：0
|
作者：
Wang S. [1 ]
Li C. [1 ]
Wang Z. [1 ]
Su Z. [1 ]
Dai F. [2 ]
机构：
[1] College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing
[2] Unit 94804 of the PLA, Shanghai
来源：
Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics | 2022年 / 44卷 / 01期
关键词：
Adaptive control; Attitude control; Carrier-based unmanned aerial vehicle (UAV); Nonlinear dynamic inversion; Power compensation;
D O I：
10.12305/j.issn.1001-506X.2022.01.27
中图分类号：
学科分类号：
摘要：
Aiming at the problem of parameter uncertainty and carrier air wake interference in the process of carrier-based unmanned aerial vehicle (UAV) landing, a carrier landing control law based on adaptive dynamic inversion is designed. The nonlinearity and multi-variable coupling are eliminated by dynamic inversion. On this basis, an adaptive law is added. The pitch attitude controller and the speed controller are designed respectively, and the Lyapunov stability principle is used to modify the adaptive law to deal with the problem of speed control under limited power, which ensures the stability of the power compensation system. The simulation results show that the control method has good dynamic performance and robustness, which can track the expected value with high accuracy in complex environments to meet the requirements of unmanned aerial vehicle(UAV) carrier landing indicators. © 2022, Editorial Office of Systems Engineering and Electronics. All right reserved.
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页码：218 / 225
页数：7
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