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Robust autopilot for a flexible missile: loop-shaping H∞ design and real ν-analysis

✍ Scribed by Jean-Patrick Friang; Gilles Duc; Jean-Paul Bonnet

Book ID: 102659208
Publisher: John Wiley and Sons
Year: 1998
Tongue: English
Weight: 818 KB
Volume: 8
Category: Article
ISSN: 1049-8923
DOI: 10.1002/(sici)1099-1239(199802)8:2<129::aid-rnc325>3.0.co;2-x

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✦ Synopsis

This paper considers the control of a bank to turn missile (developed by Aerospatiale) with very lightly damped bending modes. The autopilot is synthesized using the H loop-shaping design procedure of McFarlane and Glover. Robustness against large modelling uncertainties (including parameters and bending modes) is then investigated using the -tool, which circumvents the drawback of frequency gridding occurring in -analysis. The autopilot of the missile is finally validated on a nonlinear simulator: the performance and the robustness of the design are clearly underlined.

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