Analysis of stability for the controlled spacecraft with a deployable and retractable flexible appendage

Shaoping Shen. Analysis of stability for the controlled spacecraft with a deployable and retractable flexible appendage. In 8th IEEE International Conference on Control and Automation, ICCA 2010, Xiamen, China, June 9-11, 2010. pages 465-470, IEEE, 2010. [doi]

Abstract

Abstract is missing.