Numerical approach for solving rigid spacecraft minimum time attitude maneuvers
- 1 January 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 13 (1) , 38-45
- https://doi.org/10.2514/3.20515
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
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