H-Infinity-LTR Technique Applied to Robust Control of Propulsion-Controlled Aircraft-Reference-Cited by-同舟云学术

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H-Infinity-LTR Technique Applied to Robust Control of Propulsion-Controlled Aircraft

Published:2009-06-14 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference
language:
Short-container-title:

Author:

Hitachi Yoshitsugu¹,Liu Hugh¹

Affiliation:

1. University of Toronto Institute for Aerospace Studies

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-6176

Reference44 articles.

1. 2“AIRCRAFT ACCIDENT REPORT: UNITED AIRLINES FLIGHT 232 McDonnell Douglas DC-10-10 Sioux Gateway Airport Sioux City, Iowa July 19, 1989,” Tech. Rep. PB90-910406 NTSB/AAR-90/06, National Transportation Safety Board, 1990.

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2. Robust Control for Air-Breathing Hypersonic Cruise Vehicles;Lecture Notes in Electrical Engineering;2013

3. A Passive Fault Tolerant Flight Control for Maximum Allowable Vertical Tail Damaged Aircraft;Journal of Dynamic Systems, Measurement, and Control;2012-03-27

4. Robust Thrust-Only Control of Damaged Aircraft with Horizontal Tail Loss;AIAA Guidance, Navigation, and Control Conference;2010-06-26

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