Multi-model And Fuzzy PID Control for Fixed-wing UAV
Dali Zhou, Qingbo Geng
Available Online April 2015.
- https://doi.org/10.2991/icmra-15.2015.103How to use a DOI?
- multi-model; adaptive control; fuzzy PID; F16
- 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.
- Open Access
- This is an open access article distributed under the CC BY-NC license.
Cite this article
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 - https://doi.org/10.2991/icmra-15.2015.103 ID - Zhou2015/04 ER -