A new guidance law for homing missiles
- 1 May 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 8 (3), 402-404
- https://doi.org/10.2514/3.19994
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Missile Guidance Laws Based on Singular Perturbation MethodologyJournal of Guidance and Control, 1980
- On Optimal Guidance for Homing MissilesJournal of Guidance and Control, 1979
- An optimal terminal guidance lawIEEE Transactions on Automatic Control, 1976
- Quasi-optimum proportional navigationIEEE Transactions on Automatic Control, 1970
- Optimum intercept laws for accelerating targets.AIAA Journal, 1968