IEEE - Institute of Electrical and Electronics Engineers, Inc. - Analysis of stability for the controlled spacecraft with a deployable flexible appendage

2009 IEEE International Conference on Control and Automation (ICCA)

Author(s): Shaoping Shen
Publisher: IEEE - Institute of Electrical and Electronics Engineers, Inc.
Publication Date: 1 December 2009
Conference Location: Christchurch, New Zealand, New Zealand
Conference Date: 9 December 2009
Page(s): 1,769 - 1,774
ISBN (CD): 978-1-4244-4707-7
ISBN (Paper): 978-1-4244-4706-0
DOI: 10.1109/ICCA.2009.5410569
Regular:

In this paper we analyze the stability of the controlled spacecraft with a deployable flexible appendage. The center body of the spacecraft is controlled by PD controller. According to Lyapunov... View More

Advertisement