Pilot-in-the-Loop Evaluation of a Yaw Rate to Throttle Feedback Control with Enhanced Engine Response-Reference-Cited by-同舟云学术

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Pilot-in-the-Loop Evaluation of a Yaw Rate to Throttle Feedback Control with Enhanced Engine Response

Published:2012-08-13 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference
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Author:

Litt Jonathan¹,Guo Ten-Huei¹,Sowers T. Shane²,Chicatelli Amy²,Fulton Christopher³,May Ryan³,Owen A. Karl⁴

Affiliation:

1. NASA Glenn Research Center

2. Vantage Partners, LLC

3. Zin Technologies

4. Motile Robotics, Inc

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-5027

Reference11 articles.

1. 1Burcham, F. W., Jr., Fullerton, C. G., and Maine, T. A. "Manual Manipulation of Engine Throttles for Emergency Flight Control,"NASA/TM-2004-212045, January 2004.

2. 2Nguyen, N., and Stepanyan, V. "Flight-Propulsion Response Requirements for Directional Stability and Control," AIAA 2010-3471, AIAA Infotech@Aerospace,Atlanta, GA, April 20-22.

3. An Emergency Engine Response Requirement Analysis Tool for Lateral-Directional Dynamic Aircraft Stability

4. Flight Simulator Evaluation of Enhanced Propulsion Control Modes for Emergency Operation

Cited by 2 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. Aircraft Loss of Control Problem Analysis and Research Toward a Holistic Solution;Journal of Guidance, Control, and Dynamics;2017-04

2. Validation of Safety-Critical Systems for Aircraft Loss-of-Control Prevention and Recovery;AIAA Guidance, Navigation, and Control Conference;2012-08-13

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