A Differential Game Based Guidance Law for an Accelerating Exoatmospheric Missile
Author:
Affiliation:
1. College of Automation Engineering; Nanjing University of Aeronautics and Astronautics; Nanjing 210016 China
Funder
Funding of Jiangsu Innovation Program for Graduate Education
Publisher
Wiley
Subject
Control and Systems Engineering
Reference10 articles.
1. Optimality of proportional navigation;Kreindler;AIAA J.,1973
2. Guidance-to-collision law for an accelerating exoatmospheric interceptor missile;Reisner;J. Guid. Control Dyn.,2013
3. Development of guidance laws for a variable-speed missile;Gazit;Dynam. Control,1991
4. Exo-atmospheric guidance of an accelerating interceptor missile;Shima;J. Frank. Inst.-Eng. Appl. Math.,2012
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