Abstract

This paper addresses the problem of analyzing 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).

Original languageEnglish
Pages (from-to)8-16
Number of pages9
JournalJournal of the Institution of Engineers (India): Aerospace Engineering Journal
Volume86
Issue numberMAY
Publication statusPublished - 05-2005

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Electronic guidance systems
Robustness (control systems)
Controllers
Missiles
Specifications

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

Cite this

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title = "Robustness analysis of a typical missile guidance system",
abstract = "This paper addresses the problem of analyzing 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).",
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