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.
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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Every reasonable effort has been made to ensure that permission has been obtained for items included in DRO. If you believe that your rights have been infringed by this repository, please contact drosupport@deakin.edu.au.