pathirana-precisionmissile-2003.pdf (300.85 kB)
Precision missile guidance for systems intercepting at small attack angles : a H‡ tracking approach
conference contribution
posted on 2003-01-01, 00:00 authored by Pubudu PathiranaPubudu Pathirana, A Savkin, Saeid NahavandiThis 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 2003Event
International Conference on Computational Intelligence, Robotics and Autonomous Systems (2003 : Singapore)Publisher
CIRAS Organising CommitteeLocation
Pan Pacific Hotel, SingaporePlace of publication
SingaporeStart date
2003-12-15End date
2003-12-18Language
engNotes
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E1 Full written paper - refereedCopyright notice
2003, CIRASEditor/Contributor(s)
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