Simulation research on hypersonic vehicle based on fuzzy adaptive control

DOI

10.2991/iccia-17.2017.28How to use a DOI?

Keywords

Hypersonic vehicle, Fuzzy adaptive control, PID controller, MATLAB.

Abstract

Aiming at the control problem of hypersonic vehicle, the traditional linear control method fails to meet the expected control index, thus this paper establishes the control model of the aircraft. This paper applies the fuzzy control structure to the traditional PID controller, and through fuzzy control to adjust PID parameters in real-time to achieve adaptive control. And then by using MATLAB simulation, the influence of speed change and height change to the control of the aircraft is analyzed. The simulation results show that compared with the traditional PID control, the controller designed in this paper has higher robustness and better tracking effect.

Copyright

© 2017, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Zhouli Zhu
AU  - Wei Chen
AU  - Wei Zhou
AU  - Qun Li
PY  - 2016/07
DA  - 2016/07
TI  - Simulation research on hypersonic vehicle based on fuzzy adaptive control
BT  - Proceedings of the 2nd International Conference on Computer Engineering, Information Science & Application Technology (ICCIA 2017)
PB  - Atlantis Press
SP  - 174
EP  - 180
SN  - 2352-538X
UR  - https://doi.org/10.2991/iccia-17.2017.28
DO  - 10.2991/iccia-17.2017.28
ID  - Zhu2016/07
ER  -