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Precision missile guidance for systems intercepting at small attack angles : a H‡ tracking approach

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conference contribution
posted on 2003-01-01, 00:00 authored by Pubudu PathiranaPubudu Pathirana, A Savkin, Saeid NahavandiSaeid Nahavandi
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.

History

Title of proceedings

Proceedings of the International Conference on Computational Intelligence, Robotics and Autonomous Systems : CIRAS 2003

Event

International Conference on Computational Intelligence, Robotics and Autonomous Systems (2003 : Singapore)

Publisher

CIRAS Organising Committee

Location

Pan Pacific Hotel, Singapore

Place of publication

Singapore

Start date

2003-12-15

End date

2003-12-18

Language

eng

Notes

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Publication classification

E1 Full written paper - refereed

Copyright notice

2003, CIRAS

Editor/Contributor(s)

P Vadakkepat

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