Virtually constrained generalized relative motion modeling and a control parameter optimizer for automatic carrier landing

• Published in: Aircraft engineering Vol. 96; no. 3; pp. 448 - 457
• Main Authors: Zhang, Yiwei, Li, Daochun, Kan, Zi, Yao, Zhuoer, Xiang, Jinwu
• Format: Journal Article
• Language: English
• Published: Bradford Emerald Publishing Limited 16.04.2024; Emerald Group Publishing Limited
• Subjects: Accuracy; Aircraft; Algorithms; Automatic landing control; Design optimization; Design parameters; Flight control; Heuristic; Landing aids; Mathematical models; Optimization; Particle swarm optimization; Proportional integral derivative; Robust control; Robustness; Sliding mode control; Control parameter optimization; Virtually constrained generalized relative motion; Automatic carrier landing system; Particle swarm optimization algorithm
• ISSN: 1748-8842; 1758-4213; 1748-8842
• DOI: 10.1108/AEAT-08-2023-0217

Purpose This paper aims to propose a novel control scheme and offer a control parameter optimizer to achieve better automatic carrier landing. Carrier landing is a challenging work because of the severe sea conditions, high demand for accuracy and non-linearity and maneuvering coupling of the aircraft. Consequently, the automatic carrier landing system raises the need for a control scheme that combines high robustness, rapidity and accuracy. In addition, to exploit the capability of the proposed control scheme and alleviate the difficulty of manual parameter tuning, a control parameter optimizer is constructed. Design/methodology/approach A novel reference model is constructed by considering the desired state and the actual state as constrained generalized relative motion, which works as a virtual terminal spring-damper system. An improved particle swarm optimization algorithm with dynamic boundary adjustment and Pareto set analysis is introduced to optimize the control parameters. Findings The control parameter optimizer makes it efficient and effective to obtain well-tuned control parameters. Furthermore, the proposed control scheme with the optimized parameters can achieve safe carrier landings under various severe sea conditions. Originality/value The proposed control scheme shows stronger robustness, accuracy and rapidity than sliding-mode control and Proportion-integration-differentiation (PID). Also, the small number and efficiency of control parameters make this paper realize the first simultaneous optimization of all control parameters in the field of flight control.