Quasi-closed-form solution to the time-optimal rigid spacecraft reorientation problem
- 1 May 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 16 (3) , 453-461
- https://doi.org/10.2514/3.21031
Abstract
No abstract availableKeywords
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