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
Issue numberMAY
Publication statusPublished - 05-2005

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering


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