Deakin home > Deakin University Library > Deakin Research Online > Precision missile guidance for systems intercepting at small attack angles : a H‡ tracking approach
Openly accessible

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.

Attached Files (Some files may be inaccessible until you login with your Deakin Research Online credentials)
Name Description MIMEType Size Downloads
pathirana-precisionmissile-2003.pdf Published version application/pdf 300.84KB 78

Title Precision missile guidance for systems intercepting at small attack angles : a H‡ tracking approach
Author(s) Pathirana, Pubudu
Savkin, Andrey
Nahavandi, Saeid
Conference name International Conference on Computational Intelligence, Robotics and Autonomous Systems (2003 : Singapore)
Conference location Pan Pacific Hotel, Singapore
Conference dates 15-18 December 2003
Title of proceedings 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
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

Language eng
Field of Research 090108 Satellite, Space Vehicle and Missile Design and Testing
HERDC Research category E1 Full written paper - refereed
Copyright notice ©2003, CIRAS
Persistent URL http://hdl.handle.net/10536/DRO/DU:30005035

Document type: Conference Paper
Collections: School of Engineering and Technology
Open Access Collection
Connect to link resolver
 
Unless expressly stated otherwise, the copyright for items in Deakin Research Online is owned by the author, with all rights reserved.

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.

Versions
Version Filter Type
Access Statistics: 415 Abstract Views, 78 File Downloads  -  Detailed Statistics
Created: Mon, 07 Jul 2008, 09:44:36 EST