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Preliminary Flight Results of a Fly-by-throttle Emergency Flight Control System on an F-15 AirplaneA multi-engine aircraft, with some or all of the flight control system inoperative, may use engine thrust for control. NASA Dryden has conducted a study of the capability and techniques for this emergency flight control method for the F-15 airplane. With an augmented control system, engine thrust, along with appropriate feedback parameters, is used to control flightpath and bank angle. Extensive simulation studies were followed by flight tests. The principles of throttles only control, the F-15 airplane, the augmented system, and the flight results including actual landings with throttles-only control are discussed.
Document ID
19940008781
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Burcham, Frank W., Jr.
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Maine, Trindel A.
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Fullerton, C. Gordon
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Wells, Edward A.
(McDonnell-Douglas Automation Co. Saint Louis, MO., United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1993
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TM-4503
NAS 1.15:4503
H-1911
AIAA PAPER 93-1820
Report Number: NASA-TM-4503
Report Number: NAS 1.15:4503
Report Number: H-1911
Report Number: AIAA PAPER 93-1820
Meeting Information
Meeting: AIAA/SAE/ASME Joint Propulsion Conference
Location: Monterey, CA
Country: United States
Start Date: June 28, 1993
End Date: June 30, 1993
Accession Number
94N13254
Funding Number(s)
PROJECT: RTOP 533-02-34
Distribution Limits
Public
Copyright
Public Use Permitted.
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