Multi-model And Fuzzy PID Control for Fixed-wing UAV

DOI

10.2991/icmra-15.2015.103How to use a DOI?

Keywords

multi-model; adaptive control; fuzzy PID; F16

Abstract

This paper puts forward a kind of unmanned aerial vehicle (UAV) control method for longitudinal dynamics. Which includes velocity loop (inner loop) and height loop (outer loop). Multi-model adaptive control is used to control the velocity of UAV in the inner loop. The construction of model set and switching strategy of multi-model is introduced in this paper. Fuzzy PID is proposed to control the height of UAV in the outer loop. In this paper, we introduce the design of fuzzy rules, and use fuzzy controller to determine PID control parameters. Finally, the simulation of F16 model is carried out to verify that the improved control method is efficient and effective.

Copyright

© 2015, 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/).

Download article (PDF)

TY  - CONF
AU  - Dali Zhou
AU  - Qingbo Geng
PY  - 2015/04
DA  - 2015/04
TI  - Multi-model And Fuzzy PID Control for Fixed-wing UAV
BT  - Proceedings of the 3rd International Conference on Mechatronics, Robotics and Automation
PB  - Atlantis Press
SP  - 523
EP  - 528
SN  - 2352-538X
UR  - https://doi.org/10.2991/icmra-15.2015.103
DO  - 10.2991/icmra-15.2015.103
ID  - Zhou2015/04
ER  -