Optimal Guidance with Maneuvering Targets
- 1 March 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 11 (3) , 204-206
- https://doi.org/10.2514/3.62041
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Stability of Motion of Force-Free Spinning Satellites with Flexible AppendagesJournal of Spacecraft and Rockets, 1972
- Optimal intercept guidance for short-range tactical missilesAIAA Journal, 1971
- On the high-spin motion of a satellite containing elastic parts.Journal of Spacecraft and Rockets, 1966