Volume 47 Issue 1
Jan.  2021
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BI Daoming, HUANG Hui, FAN Jing, et al. Nonlinear moving path following control and its application to carrier landing[J]. Journal of Beijing University of Aeronautics and Astronautics, 2021, 47(1): 45-55. doi: 10.13700/j.bh.1001-5965.2019.0646(in Chinese)
Citation: BI Daoming, HUANG Hui, FAN Jing, et al. Nonlinear moving path following control and its application to carrier landing[J]. Journal of Beijing University of Aeronautics and Astronautics, 2021, 47(1): 45-55. doi: 10.13700/j.bh.1001-5965.2019.0646(in Chinese)

Nonlinear moving path following control and its application to carrier landing

doi: 10.13700/j.bh.1001-5965.2019.0646
Funds:

Beijing Natural Science Foundation 4202038

Beijing Natural Science Foundation 4172070

National Natural Science Foundation of China 61827901

More Information
  • Corresponding author: ZHENG Zewei, E-mail:zeweizheng@buaa.edu.cn
  • Received Date: 24 Dec 2019
  • Accepted Date: 03 Feb 2020
  • Publish Date: 20 Jan 2021
  • This paper proposes a novel Moving Path Following (MPF) control method by improving the time-varying vector field method. Moreover, it is applied to the automatic carrier landing problem of carrier-based aircraft. Based on the nonlinear model of carrier-based aircraft, backstepping method is used as the main frame. Besides, the path following error is defined in the time-varying vector field. In addition, Lyapunov function is designed for the defined virtual control variable to achieve fast and accurate tracking for the heading angle and the climb angle, and the path of the aircraft is ensured to follow the desired moving path. The stability analysis proves that the following error converges to a small region, and the simulation results show that the control method has good performance in carrier landing.

     

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