Optimal feedback slewing of flexible spacecraft

• 1 September 1981
• journal article
• Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance and Control
• Vol. 4  (5) , 472-479
• https://doi.org/10.2514/3.19749

Abstract

Keywords

• FLEXIBLE SPACECRAFT
• OPTIMAL FEEDBACK SLEWING
• SLEWING OF FLEXIBLE