Research on Attitude Control of Spacecraft Based on ADRC

Abstract:

Article Preview

Modern spacecraft demands from an attitude control system very high performance and accuracy, and many new features, such as disturbance rejection capability. The recently developed active disturbance rejection control technology is applied to the attitude control of spacecraft subject to disturbances and parametric uncertainties. Simulation and experiment show significant advantages of the proposed attitude controller over the controller resulting from conventional PID approach.

Info:

Periodical:

Advanced Materials Research (Volumes 383-390)

Edited by:

Wu Fan

Pages:

358-365

DOI:

10.4028/www.scientific.net/AMR.383-390.358

Citation:

F. L. Teng et al., "Research on Attitude Control of Spacecraft Based on ADRC", Advanced Materials Research, Vols. 383-390, pp. 358-365, 2012

Online since:

November 2011

Export:

Price:

$35.00

In order to see related information, you need to Login.

In order to see related information, you need to Login.