Reconfigurable Controls for Rotorcraft — A Feasibility Study-Reference-Cited by-同舟云学术

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Reconfigurable Controls for Rotorcraft — A Feasibility Study

Published:1997-07-01 Issue:3 Volume:42 Page:254-263
ISSN:2161-6027
Container-title:Journal of the American Helicopter Society
language:en
Short-container-title:j am helicopter soc

Author:

Heiges Michael W.

Publisher

American Helicopter Society

Cited by 11 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Fault-Tolerant Control on a UH-60 Black Hawk helicopter using horizontal stabilator;CEAS Aeronautical Journal;2020-10-06

2. Horizontal Stabilator Utilization for Post Swashplate Failure Operation on a UH-60 Black Hawk Helicopter;Journal of the American Helicopter Society;2020-04-01

3. A Framework for Robust Rotorcraft Flight Control Design;Journal of the American Helicopter Society;2011-04-01

4. Bibliographical review on reconfigurable fault-tolerant control systems;Annual Reviews in Control;2008-12

5. Survivability of helicopter with individual blade primary control failure;The Aeronautical Journal;2007-10

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