Frequency-shaped large-angle maneuvers
Author:
Affiliation:
1. Cambridge Research Associates, MA
2. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1987-174
Reference26 articles.
1. Optimal nonlinear feedback control for spacecraft attitude maneuvers
2. Chun, H.M. "Large-Angle Slewing Maneuvers for Flexible Spacecraft," Doctoral Dissertation,Massachusetts Institute of Technology, Cambridge, Massachuietts, 1986.
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3. Exact minimum-time control of a distributed system using a traveling wave formulation;Journal of Optimization Theory and Applications;1992-04
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