Article ID Journal Published Year Pages File Type
709215 IFAC Proceedings Volumes 2013 5 Pages PDF
Abstract

Rendezvous and docking is a key operational technology for human beings to explore and use space. In November 2011 and June 2012, China achieved successful automatic and manual rendezvous and docking between Shenzhou-8, Shenzhou-9 and Tiangong-1, respectively. The control difficulty of these rendezvous and docking lies in flexible vibration of solar panels, cross-coupling between attitude and position control, and serious disturbances caused by thrusters’ plume. To solve these problems, an intelligent adaptive control method is proposed based on a characteristic model based intelligent adaptive control theory. Combined with a proper thruster control allocation algorithm, the on-orbit application of this control method has gained a complete success. This paper will concentrate on the basic principle, design method, theoretical analysis and on-orbit application of this intelligent adaptive control method. And the application of this method in future rendezvous and docking tasks and other spacecraft control projects will be discussed.

Related Topics
Physical Sciences and Engineering Engineering Computational Mechanics