Fighter evasive maneuvers against proportional navigation missile
Author:
Affiliation:
1. Mitsubishi Electric Corporation, Tokyo, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45388
Reference9 articles.
1. Proportional navigation vs an optimally evading, constant-speed target in two dimensions
2. Optimal evasive tactics against a proportional navigation missile with time delay.
3. Analysis of Three-Dimensional Optimal Evasion with Linearized Kinematics
4. The effects of non-linear kinematics in optimal evasion
5. Comparison of Optimal Control and Differential Game Intercept Missile Guidance Laws
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