Abstract:
The purpose of the paper is to present main results about design and simulation of an attitude orbit controller for a solar sail spacecraft with large flimsy appendages. ...Show MoreMetadata
Abstract:
The purpose of the paper is to present main results about design and simulation of an attitude orbit controller for a solar sail spacecraft with large flimsy appendages. The presence of a large number of uncertain flexible modes makes this problem suited for a robust control design based on quantitative feedback theory.
Date of Conference: 14-17 December 2004
Date Added to IEEE Xplore: 16 May 2005
Print ISBN:0-7803-8682-5
Print ISSN: 0191-2216
Contents 