Maximum-information guidance for homing missiles
- 1 July 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 8 (4), 494-497
- https://doi.org/10.2514/3.20010
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Adaptive noise estimation for homing missilesJournal of Guidance, Control, and Dynamics, 1984