Multirate H-infinity loop-shaping control applied to missile autopilot design-Reference-Cited by-同舟云学术

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Multirate H-infinity loop-shaping control applied to missile autopilot design

Published:2001-08-06 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference and Exhibit
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Author:

Harcaut J.¹,Farret D.¹,Duc G.¹

Affiliation:

1. Ecole Superieure D'Electricite, Gif-sur-Yvette, France

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-4283

Reference17 articles.

1. G.E. Dullerud, S.G. Lall, «Analysis and Synthesis Tools for Time-varying Systems)), 36thIEEE Conf. On Decision and Control, pp.4543-4548,SanDiego,1997.

2. S.G.Lall, G.E.Dullerud, «Hoo Synthesis for Multi-rate Hybrid Systems », 36thIEEE Conf. On Decision and Control, pp.2035-2040, San Diego, 1997.

3. Automatica prize paper awards 1993

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