Articles

Knowledge-based intelligent pigeon-inspired optimization of carrier-based aircraft landing control

  • Dapeng ZHOU ,
  • Xiaolei QU
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  • 1.Flight Control Department,Shenyang Aircraft Design & Research Institute,Shenyang 110035,China
    2.School of Automation,Northwestern Polytechnical University,Xi’an 710072,China

Received date: 2024-06-06

  Revised date: 2024-07-19

  Accepted date: 2024-08-19

  Online published: 2024-09-02

Supported by

Liaoning Provincial National Science and Technology Award Project(2022JH25/10200002)

Abstract

Aiming at the problem of automatic landing of carrier-based aircraft under deck motion and airflow disturbance, a longitudinal landing control law design method based on dynamic inverse control is proposed. The carrier-based aircraft model, deck motion model and stern flow disturbance model are established, and the dynamic inverse control method of carrier-based aircraft landing is designed to estimate the first-order derivative of the reference command within a finite time. An knowledge-based intelligent pigeon-inspired optimization algorithm is proposed to iteratively optimize the parameters of the dynamic inverse controller, which can improve the command following accuracy of carrier-based aircraft landing. The MATLAB Simulink simulation environment is used to simulate and verify the proposed automatic landing control system of carrier-based aircraft. By comparing with pigeon-inspired optimization algorithm and particle swarm optimization algorithm, it is shown that the superiority of the carrier-based aircraft landing control method of knowledge-based intelligent pigeon-inspired optimization, which can significantly improve the accuracy and speed of carrier-based aircraft attitude control, meet the requirements of carrier-based aircraft landing, and has good robustness.

Cite this article

Dapeng ZHOU , Xiaolei QU . Knowledge-based intelligent pigeon-inspired optimization of carrier-based aircraft landing control[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2024 , 45(S1) : 730801 -730801 . DOI: 10.7527/S1000-6893.2024.30801

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