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The problem of precision missile guidance: LQR and H∞ control frameworks

Savkin, Andrey V., Pathirana, Pubudu N. and Faruqi, Farhan A. 2003, The problem of precision missile guidance: LQR and H∞ control frameworks, in Proceedings of the 40th IEEE Conference on Decision and Control, IEEE, Piscataway, N.J., pp. 1535-1540, doi: 10.1109/TAES.2003.1238744.

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Title The problem of precision missile guidance: LQR and H∞ control frameworks
Author(s) Savkin, Andrey V.
Pathirana, Pubudu N.ORCID iD for Pathirana, Pubudu N. orcid.org/0000-0001-8014-7798
Faruqi, Farhan A.
Conference name Decision and Control. IEEE Conference (40th : 2001 : Orlando, Florida)
Conference location Orlando, Florida
Conference dates 2001/12/04 - 2001/12/07
Title of proceedings Proceedings of the 40th IEEE Conference on Decision and Control
Publication date 2003
Start page 1535
End page 1540
Total pages 10
Publisher IEEE
Place of publication Piscataway, N.J.
Summary The paper addresses the precision missile guidance problem where the successful intercept criterion has been defined in terms of both minimizing the miss distance and controlling the missile body attitude with respect to the target at the terminal point. We show that the H∞ control theory when suitably modified provides an effective framework for the precision missile guidance problem. Existence of feedback controllers (guidance laws) is investigated for the case of finite horizon and non-zero initial conditions. Both state feedback and output feedback implementations are explored.
ISSN 0191-2216
Language eng
DOI 10.1109/TAES.2003.1238744
Field of Research 090699 Electrical and Electronic Engineering not elsewhere classified
Socio Economic Objective 0 Not Applicable
HERDC Research category E1.1 Full written paper - refereed
Copyright notice ©2003, IEEE
Persistent URL http://hdl.handle.net/10536/DRO/DU:30096285

Document type: Conference Paper
Collection: School of Engineering
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