Research on Single Channel Rolling Control for Fixed Canard Rudder

Article Preview

Abstract:

According to the rotate speed switching problems of rapidity and stability during single channel rolling control for fixed canard rudder, the control algorithm based on active disturbance rejection controller (ADRC) was presented to control the rudders rotate speed switching. The working principle of fixed canard rudder was analyzed, and the mathematical model of the rudder was established, and the ADRC cascade controller for the rudder was designed. The simulation results indicates that not only the proposed rotate speed switching control strategy for the rudder is feasible, but also the proposed ADRC algorithm improves the rapidity of speed switching process, with switching time of 30ms, no overshoot, and very good robustness under inner perturbation and external disturbance with nonlinear friction considered.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

1150-1153

Citation:

Online since:

October 2013

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2013 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] Cui Yebing, Ju Yutao, Zheng Jian . Research on dual mode control for electric servo mechanism of thrust vector control. Journal of Solid Rocket Technology. 2012; 35(5): 688-693.

Google Scholar

[2] Yohan Lin and Ethan Baumann. Tests and Techniques for Characterizing and Modeling X-43A Electromechanical Actuators. NASA/TM-2008-214637.

Google Scholar

[3] Dr. Erland Ørbekk. SuperSonic Split Line TVC Technology and Testing at Nammo Raufoss AS. In: 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 9-12 July 2006, Sacramento, California; AIAA Journal, 2006-4940.

DOI: 10.2514/6.2006-4940

Google Scholar

[4] GUO Hong, XING Wei. Development of Electromechanical Actuators. Acta Aeronautica Et Astronautica Sinica 2007; 28(3), 1000-6893.

Google Scholar

[5] X. Shi, S. Chang, Precision motion control of a novel electromagnetic linear actuator based on a modified active disturbance rejection controller. Proc. IMechE, Part I: J. Syst. Control Eng. 2012; 226 (5): 606-614.

DOI: 10.1177/0959651811430036

Google Scholar

[6] Jean-Francois Guery, I-Shih Chang, Toru Shimada. Solid propulsion for space applications: An updated roadmap. Acta Astronautica 66 (2010) 201-219.

DOI: 10.1016/j.actaastro.2009.05.028

Google Scholar

[7] Cui Yebing, Ju Yutao, Zhou Changsheng. One Feasibility of High Bandwidth Four Rudder Wings Electromechanical Actuator . Electric Machines and Control. 2012; 32(12): 92-97.

Google Scholar

[8] J. Han. Active disturbance rejection control technique, first ed. National Defense Industry Press, Beijing, (2008).

Google Scholar