Design and Evaluation of a Three-Dimensional Optimal Ascent Guidance Algorithm
- 1 November 1998
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 21 (6) , 867-875
- https://doi.org/10.2514/2.4350
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
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- Hybrid approach to near-optimal launch vehicle guidanceJournal of Guidance, Control, and Dynamics, 1994
- Rapid near-optimal aerospace plane trajectory generation and guidanceJournal of Guidance, Control, and Dynamics, 1991