Precision missile guidance for systems intercepting at small attack angles : a H‡ tracking approach
Pathirana, Pubudu, Savkin, Andrey and Nahavandi, Saeid 2003, Precision missile guidance for systems intercepting at small attack angles : a H‡ tracking approach, in Proceedings of the International Conference on Computational Intelligence, Robotics and Autonomous Systems : CIRAS 2003, CIRAS Organising Committee, Singapore.
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Proceedings of the International Conference on Computational Intelligence, Robotics and Autonomous Systems : CIRAS 2003
Editor(s)
Vadakkepat, Prahlad
Publication date
2003
Publisher
CIRAS Organising Committee
Place of publication
Singapore
Summary
This paper uses the H1 tracking ideas in the missile guidance problem. The controller performs as a Precision guidance controller for small desired attack angles although theoretically the formulas are valid (when intercepting a maneuvering target in a precision guidance point of view) only for the case of head on collision. The controller essentially navigates the missile in a unique relative arc that is de ned by the missile and target location and the desired attack angle.
Notes
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Language
eng
Field of Research
090108 Satellite, Space Vehicle and Missile Design and Testing
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