Optimal planar evasive aircraft maneuvers against proportional navigation missiles
Author:
Affiliation:
1. Singapore Technologies Aerospace, Ltd., Paya Lebar 1953, Singapore
2. Iowa State University, Ames, Iowa 50011-3231
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.21773
Reference18 articles.
1. Aircraft Missile Avoidance
2. Proportional navigation vs an optimally evading, constant-speed target in two dimensions
3. Optimal evasive tactics against a proportional navigation missile with time delay.
4. Analysis of Optimal Evasive Maneuvers Based on a Linearized Two-Dimensional Kinematic Model
5. Analysis of Three-Dimensional Optimal Evasion with Linearized Kinematics
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