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Robustness Analysis of a Typical Missile Guidance System

George, V I and Kurian, Ciji Pearl (2005) Robustness Analysis of a Typical Missile Guidance System. Journal of the Institution of Engineers (India). Aerospace Engg, 86. pp. 8-16. ISSN 0257-3423

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Abstract

This paper addresses the problem of analysing and designing a robust controller for a missile (non-minimum phase plant). This study comprises three parts, namely, (i) designing the controller in the H mixed frame work (which satisfies the criteria of both robust performance and robust Stability), (ii) modification of the above controller design by making use of the theory of H parameter space method (which is a graphical interactive method), and (iii) robust controller (which satisfies both time domain . and frequency domain specifications in the controller parameter region).

Item Type: Article
Uncontrolled Keywords: Missiles; Robust performance; Robust stability; Robust controller
Subjects: Engineering > MIT Manipal > Electrical and Electronics
Engineering > MIT Manipal > Instrumentation and Control
Depositing User: MIT Library
Date Deposited: 12 Jan 2012 11:16
Last Modified: 12 Jan 2012 11:16
URI: http://eprints.manipal.edu/id/eprint/2456

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