Design and simulation verification of height control of aircraft based on experimental system

Lingling Wang; Jin Yu

doi:10.1117/12.2635216

25 April 2022 Design and simulation verification of height control of aircraft based on experimental system

Lingling Wang, Jin Yu

Proceedings Volume 12244, 2nd International Conference on Mechanical, Electronics, and Electrical and Automation Control (METMS 2022); 1224438 (2022) https://doi.org/10.1117/12.2635216
Event: 2nd International Conference on Mechanical, Electronics, and Electrical and Automation Control (METMS 2022), 2022, Guilin, China

Abstract

Designing a stable attitude control algorithm is an eternal topic in aircraft control. Based on solving such problems, the model of UAV ontology of the experimental system was simplified in this paper firstly, and then three groups of feature points was selected on the basis of the simplified model. Secondly, analysis and parameter selections of each layer of the height control loop were carried out with the idea of root locus. Finally, the computer simulation experiment was carried out on the algorithm of the designed height control system. It was shown from the experimental results that the designed algorithm is stable and reliable.

Citation Download Citation

Lingling Wang and Jin Yu "Design and simulation verification of height control of aircraft based on experimental system", Proc. SPIE 12244, 2nd International Conference on Mechanical, Electronics, and Electrical and Automation Control (METMS 2022), 1224438 (25 April 2022); https://doi.org/10.1117/12.2635216

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