Limitations of performance of a missile homing system

Pham, H, Hill, R and Bucco, D 2004, 'Limitations of performance of a missile homing system', in R. Evans and I. Mareels (ed.) Proceedings of the Fifth Asian Control Conference, Melbourne, Australia, 20-23 July 2004.


Document type: Conference Paper
Collection: Conference Papers

Title Limitations of performance of a missile homing system
Author(s) Pham, H
Hill, R
Bucco, D
Year 2004
Conference name Fifth Asian Control Conference
Conference location Melbourne, Australia
Conference dates 20-23 July 2004
Proceedings title Proceedings of the Fifth Asian Control Conference
Editor(s) R. Evans
I. Mareels
Publisher University of Melbourne
Place of publication Melbourne
Abstract This paper would investigate fundamental limitations on the dynamic performance of a missile homing system. A linearized model of a proportional navigation guidance and control loop is shown in the block diagram below. This linear time-varying system is investigated in the paper. An important factor in the design of control systems is time-domain response to external inputs. Recent theoretical work on linear time-invariant system limitations is extended to linear time-varying systems, and is applied to the problem of determining the smallest miss distance achievable using a controller in the loop. This is formulated as a convex minimization problem. Application is made to the effect of hard limits on allowable missile acceleration on the final miss distance.
Subjects Optimisation
Keyword(s) optimisation
design of control systems
convex minimisation
Copyright notice © 2004 IEEE
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