IEEE - Institute of Electrical and Electronics Engineers, Inc. - Robust pseudo-linearising autopilot for a quasi-linear parameter varying missile model

Proceedings of 2000 American Control Conference (ACC 2000)

Author(s): Tsourdos, A. ; Zbikowski, R. ; White, B.A.
Publisher: IEEE - Institute of Electrical and Electronics Engineers, Inc.
Publication Date: 1 January 2000
Conference Location: Chicago, IL, USA
Conference Date: 28 June 2000
Volume: 6
ISBN (Paper): 0-7803-5519-9
ISSN (Paper): 0743-1619
DOI: 10.1109/ACC.2000.876988
Regular:

A sideslip velocity autopilot is designed for a model of a tactical missile and robust stability of the closed-loop system investigated. The tail-controlled missile in the cruciform fin... View More

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