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Pilot-in-the-Loop Evaluation of a Yaw Rate to Throttle Feedback Control with Enhanced Engine ResponseThis paper describes the implementation and evaluation of a yaw rate to throttle feedback system designed to replace a damaged rudder. It can act as a Dutch roll damper and as a means to facilitate pilot input for crosswind landings. Enhanced propulsion control modes were implemented to increase responsiveness and thrust level of the engine, which impact flight dynamics and performance. Piloted evaluations were performed to determine the capability of the engines to substitute for the rudder function under emergency conditions. The results showed that this type of implementation is beneficial, but the engines' capability to replace the rudder is limited.
Document ID
20150006756
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Litt, Jonathan S.
(NASA Glenn Research Center Cleveland, OH, United States)
Guo, Ten-Huei
(NASA Glenn Research Center Cleveland, OH, United States)
Sowers, T. Shane
(Vantage Partners, LLC Brook Park, OH, United States)
Chicatelli, Amy K.
(Vantage Partners, LLC Brook Park, OH, United States)
Fulton, Christopher E.
(Zin Technologies, Inc. Cleveland, OH, United States)
May, Ryan D.
(Vantage Partners, LLC Brook Park, OH, United States)
Owen, A. Karl
(Motile Robotics Joppa, MD, United States)
Date Acquired
April 27, 2015
Publication Date
August 13, 2012
Subject Category
Aircraft Stability And Control
Aircraft Propulsion And Power
Report/Patent Number
AIAA Paper 2012-5027
E-663889
Report Number: AIAA Paper 2012-5027
Report Number: E-663889
Meeting Information
Meeting: AIAA Guidance Navigation and Control Conference
Location: Minneapolis, MN
Country: United States
Start Date: August 13, 2012
End Date: August 16, 2012
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 284848.02.05.03.02.03
Distribution Limits
Public
Copyright
Public Use Permitted.
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