Receding Horizon Guidance Laws with No Information on the Time-to-Go
- 1 March 2000
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 23 (2), 193-199
- https://doi.org/10.2514/2.4518
Abstract
No abstract availableKeywords
This publication has 13 references indexed in Scilit:
- Closed-form optimal guidance law for missiles of time-varying velocityJournal of Guidance, Control, and Dynamics, 1996
- Optimal guidance for high-order and acceleration constrained missileJournal of Guidance, Control, and Dynamics, 1991
- An analysis of modern versus classical homing guidanceIEEE Transactions on Aerospace and Electronic Systems, 1990
- Performance analysis of PNG laws for randomly maneuvering targetsIEEE Transactions on Aerospace and Electronic Systems, 1990
- Estimation of the time-to-go parameter for air-to-air missilesJournal of Guidance, Control, and Dynamics, 1985
- A New Look at Classical vs Modern Homing Missile GuidanceJournal of Guidance and Control, 1981
- An optimal terminal guidance lawIEEE Transactions on Automatic Control, 1976
- Optimal Guidance with Maneuvering TargetsJournal of Spacecraft and Rockets, 1974
- Optimal intercept guidance for short-range tactical missilesAIAA Journal, 1971
- Optimum intercept laws for accelerating targets.AIAA Journal, 1968