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Linear-quadratic regulator controller design for quadrotor based on pigeon-inspired optimization

Yongbin Sun (School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing, China)
Ning Xian (School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing, China)
Haibin Duan (School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing, China)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 3 October 2016

411

Abstract

Purpose

The purpose of this paper is to propose a new algorithm for linear-quadratic regulator (LQR) controller of a quadrotor with fast and stable performance, which is based on pigeon-inspired optimization (PIO).

Design/methodology/approach

The controller is based on LQR. The determinate parameters are optimized by PIO, which is a newly proposed swarm intelligent algorithm inspired by the characteristics of homing pigeons.

Findings

The PIO-optimized LQR controller can obtain the optimized parameters and achieve stabilization in about 3 s.

Practical implications

The PIO-optimized LQR controller can be easily applied to the flight formation, autonomous aerial refueling (AAR) and detection of unmanned aerial vehicles, especially applied to (AAR) in this paper.

Originality/value

This research applies PIO to optimize the tuning parameters of LQR, which can considerably improve the fast and stabilizing performance of attitude control. The simulation results show the effectiveness of the proposed algorithm.

Keywords

Acknowledgements

This work was partially supported by National Natural Science Foundation of China under Grant Nos 61425008, 61333004 and 61273054, and Aeronautical Foundation of China under Grant No. 20135851042.

Citation

Sun, Y., Xian, N. and Duan, H. (2016), "Linear-quadratic regulator controller design for quadrotor based on pigeon-inspired optimization", Aircraft Engineering and Aerospace Technology, Vol. 88 No. 6, pp. 761-770. https://doi.org/10.1108/AEAT-03-2015-0088

Publisher

:

Emerald Group Publishing Limited

Copyright © 2016, Emerald Group Publishing Limited

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