Abstract
A mathematical model is established for the self-designed vehicle test simulation attitude control system. On the basis of designing LQR controller based on linear quadratic optimal control method, Particle swarm optimization is used to optimize the parameter matrix of LQR controller. In order to stabilize the attitude control of the aircraft, reduce the response time and frequency of the system. Simulation experiment proves: The stability of the system is improved by the optimized LQR controller using particle swarm optimization, got a good control effect, it has high practical application value.
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Acknowledgments
Jilin provincial education department project «Automatic brake device design of automobile intelligent anti – error» (project number: JJKH2017162KJ). Supported by Program for Innovative Research Team of JiLin Engineering Normal University.
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Fang, J., Li, W. (2019). Design of LQR Controller Based on Particle Swarm Optimization Algorithm for Aircraft Test Simulation Attitude Control System. In: Abawajy, J., Choo, KK., Islam, R., Xu, Z., Atiquzzaman, M. (eds) International Conference on Applications and Techniques in Cyber Security and Intelligence ATCI 2018. ATCI 2018. Advances in Intelligent Systems and Computing, vol 842. Springer, Cham. https://doi.org/10.1007/978-3-319-98776-7_150
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DOI: https://doi.org/10.1007/978-3-319-98776-7_150
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