Constrained Impulsive Trajectory Optimization for Orbit-to-Orbit Transfer
- 1 May 1979
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance and Control
- Vol. 2 (3), 204-212
- https://doi.org/10.2514/3.55862
Abstract
No abstract availableKeywords
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