New results in optimal missile avoidance analysis
- 1 September 1994
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 17 (5) , 897-902
- https://doi.org/10.2514/3.21287
Abstract
No abstract availableKeywords
This publication has 9 references indexed in Scilit:
- Optimal evasion against a proportionally guided pursuerJournal of Guidance, Control, and Dynamics, 1989
- State-dependent optimality of a singular subarcAutomatica, 1988
- Fighter evasive maneuvers against proportional navigation missileJournal of Aircraft, 1986
- The effects of non‐linear kinematics in optimal evasionOptimal Control Applications and Methods, 1983
- Analysis of Three-Dimensional Optimal Evasion with Linearized KinematicsJournal of Guidance and Control, 1979
- Analysis of Optimal Evasive Maneuvers Based on a Linearized Two-Dimensional Kinematic ModelJournal of Aircraft, 1977
- Optimal evasive tactics against a proportional navigation missile with time delay.Journal of Spacecraft and Rockets, 1973
- Proportional navigation vs an optimally evading, constant-speed target in two dimensionsJournal of Spacecraft and Rockets, 1970
- Fundamentals of proportional navigationIEEE Spectrum, 1966