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Vol. 160, Issue 12, December 2013, pp. 619-626

 

Bullet

 

Passivity-Based Spacecraft Attitude Control with Disturbance Suppression
 
Lina WANG, Bing WANG, Zhi LI

Department of Communication Engineering, School of Computer and Communication Engineering, University of Science and Technology Beijing, No. 30 Xueyuan Road, Haidian District, Beijing, 100083, P. R. China
Tel.: +86 10 62332873, fax: +86 10 62332873
E-mail: wln_ustb@126.com

 

Received: 18 September 2013   /Accepted: 22 November 2013   /Published: 30 December 2013

Digital Sensors and Sensor Sysstems

 

Abstract: The stability of rigid spacecraft attitude is considered. The mathematical model of spacecraft system is described by quaternion. The robust nonlinear attitude controller without angular velocity measurement is designed based on passivity-based approach. The designed attitude controller has no information related to system parameters. So it has robustness to model error and uncertainty of model parameters. The stability of spacecraft attitude control with considering external disturbance can be proved by applying Lyapunov approach and LaSalle Invariance Principle. Numerical simulation results demonstrate the effectiveness of the designed attitude controller.

 

Keywords: Attitude control, Passivity, Quaternion, External disturbance.

 

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