Time-to-go prediction for homing missiles based on minimum-time intercepts
- 1 September 1991
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 14 (5), 865-871
- https://doi.org/10.2514/3.20725
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Linear-quadratic guidance law for dual control of homing missilesJournal of Guidance, Control, and Dynamics, 1990
- Estimation of the time-to-go parameter for air-to-air missilesJournal of Guidance, Control, and Dynamics, 1985