An optimal maneuver control method for the spacecraft with flexible appendages
Author:
Affiliation:
1. Harbin Institute of Technology, People's Republic of China
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1988-4255
Reference5 articles.
1. Breakwell,J.A., Optimal feedback Slewing of Flexible Spacecraft. Jour. of Guidance and ControlVol.4. No.5 September-october 1981. pp.472-479
2. T.kida, I. Yamaguchi, Y.Ohkami, KHirako and H.Soga, An Optimal Slewing Maneuver Approach for a Class of Spacecraft with Flexible Appendages . IAF-85-227.
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