IEEE - Institute of Electrical and Electronics Engineers, Inc. - Sliding Mode Attitude and Vibration Control of Flexible Spacecraft with Actuator Dynamics

2007 IEEE International Conference on Control and Automation, ICCA 2007

Author(s): Qinglei Hu ; Lihua Xie ; Youyi Wang
Publisher: IEEE - Institute of Electrical and Electronics Engineers, Inc.
Publication Date: 1 May 2007
Conference Location: Guangzhou, China
Conference Date: 30 May 2007
Page(s): 410 - 415
ISBN (CD): 978-1-4244-0818-4
ISBN (Paper): 978-1-4244-0817-7
DOI: 10.1109/ICCA.2007.4376390
Regular:

This paper presents a dual-stage control system design method for the three-axis-rotational maneuver control and vibration stabilization of a spacecraft with flexible appendages embedded... View More

Advertisement