Techniques for developing approximate optimal advanced launch system guidance
- 1 September 1994
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 17 (5) , 889-896
- https://doi.org/10.2514/3.21286
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Approximate optimal atmospheric guidance law for aeroassisted plane-change maneuversJournal of Guidance, Control, and Dynamics, 1990
- An Approach to Optimal Guidance of an Advanced Lauch Vehicle ConceptPublished by Institute of Electrical and Electronics Engineers (IEEE) ,1990