Longitudinal automatic carrier landing system guidance law using model predictive control with an additional landing risk term

Author:

Wang Lipeng12,Zhang Zhi1,Zhu Qidan1,Dong Ran3

Affiliation:

1. College of Automation, Harbin Engineering University, Harbin, People's Republic of China

2. Science and Technology Research Institute, Harbin Engineering University, Harbin, People's Republic of China

3. Aviation System Research Department, SERI, Beijing, People’s Republic of China

Abstract

This paper used a model predictive control with an additional term to develop a modified longitudinal guidance law to reduce landing risk in an automatic carrier landing system. The landing risk model was established by using a longitudinal trajectory and touchdown point predictive principle. A traditional MPC was then involved in designing a modified automatic carrier landing system guidance law for the proposed model. The nonlinear landing mathematic model of an F/A-18 carrier-based aircraft was initially established. Considering the processed procedure in the model predictive control algorithm, the corresponding linear landing model was derived on the basis of the equilibrium states of the F/A-18. Second, landing trajectory in the longitudinal plane was analysed so that the predictive principle of the trajectory trend was reasonably addressed. Depending on the experimental sample data of a pilot model, some linear imitating envelopes are transformed from the corresponding nonlinear trajectory clusters. Furthermore, a touchdown point prediction model was further established based on the predicted trajectory and touchdown point. Third, the traditional model predictive control was introduced to integrate the landing risk term in the performance cost function to develop a novel modified algorithm that not only guides the aircraft to automatically approach and land on the carrier, but also eliminates landing risk during the final carrier approach. Linear matrix inequalities were imported to substitute algebraic inequalities derived from this new algorithm to increase calculating speed. A simulation mission was conducted on a semi-physical platform and compared with the traditional model predictive control without the additional term. The theoretical results validated the correctness and robustness of the modified algorithm and its capability to eliminate landing risk during terminal carrier approach.

Publisher

SAGE Publications

Subject

Mechanical Engineering,Aerospace Engineering

Cited by 9 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Automatic landing of carrier-based aircraft based on a collaboration of fault reconstruction and fault-tolerant control;Aerospace Science and Technology;2024-01

2. Longitudinal Landing Risk Situation Model and Suppression Based on Cloud Model and MPC;2023 IEEE International Conference on Mechatronics and Automation (ICMA);2023-08-06

3. Lateral Automatic Landing Control System for Cooperating to Suppress Risk and Deviations Based on MPC and NN;International Journal of Control, Automation and Systems;2023-05-06

4. Knowledge Graph of Civil Aircraft Approach and Landing Flight Safety Research Based on Citespace Sustainability Analysis;2022 IEEE 4th International Conference on Civil Aviation Safety and Information Technology (ICCASIT);2022-10-12

5. Automatic Carrier Landing System With Fixed Time Control;IEEE Transactions on Aerospace and Electronic Systems;2022-08

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