Attitude Decoupling Controller Design of Dual-Ducted SUAV Based on ADRC System

Article Preview

Abstract:

This dual-ducted SUAV is a nonlinear and strong coupling of multiple-input and multiple-output system, and particularly between the pitch and roll channels channel coupling is strong, in order to implement effective control, it must be decoupled. The traditional methods are difficult to achieve effective control of the strong coupling of multivariable systems. For the SUAV model of nonlinear coupling characteristics, based on the establishment of the UAV attitude model, this paper designed an attitude ADRC decoupling controller. The simulation showed this ADRC decoupling controller had strong robustness and immunity, and solved the channels coupling between the pitch and roll.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

1143-1148

Citation:

Online since:

April 2014

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2014 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] Bowen Nie, Hongxu Ma, Jian Wang, Jianwen Wang, Study on actualities and critical technologies of micro/mini quadrotor, Electronics Optics & Control. 6(2007) 113-117.

Google Scholar

[2] Junsheng Wang, Hongxu Ma, Wenlan Can, Haitao Shui, Bowen Nie, Research on Micro Quadrotor Control Based on ADRC, Journal of Projectiles , Rocket s , Missiles and Guidance. 28 (2008) 31-40.

Google Scholar

[3] Haiyan Hu, Min Xu, Active Disturbance Rejection Control of Attitude Stability for UAV Flight Control System, Journal of Telemetry,Tracking and Command. 3 (2012) 62-67.

Google Scholar

[4] Lini Zhou, Guojin Tang, Haiyang Li, Active disturbance rejection controller design for spacecraft attitude maneuver, Systems Engineering and Electronics. 12 (2007) 2122-2126.

Google Scholar

[5] Yan Pen, Mei Liu, Jun Luo, Shaorong Xie, Research on linear adaptive disturbance rejection control method for yaw tracking of unmanned rotorcraft, Chinese Journal of Scientific Instrument. 8 (2013) 1894-(1900).

Google Scholar

[6] Benallegue A, Mokhtari A, High-order sliding-mode observer for a quadrotor UAV, International Journal of Robust and Nonlinear Control. 18 (2008) 427-440.

DOI: 10.1002/rnc.1225

Google Scholar

[7] Raffo G V, Ortrga M G. An integral predictive/non-linear Hcontrol structure for a quadrotor helicopter, Automatica. 46 (2010) 29-39.

Google Scholar

[8] Voos H, Nonlinear state-dependent riccati equation control of a quadrotor UAV, in: Proceedings of the 2006 IEEE International Conference on Control Applications, Munich, Germany, 2006 , pp.2547-2552.

DOI: 10.1109/cca.2006.285869

Google Scholar

[9] Ping Jiang, Jingyu Hao, Xiaoping Zong, Peiguang Wang, Modeling and Simulation of Active Disturbances Rejection Controller Based on Simulink, Control Theory and Applications. 2 (2010) 1-4.

Google Scholar

[10] Jingqing Han, Active Disturbance Rejection Control Technique, National Defence Industry Press, Bei Jing, (2008).

Google Scholar