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Flight Testing and Simulation of an F-15 Airplane Using Throttles for Flight ControlFlight tests and simulation studies using the throttles of an F-15 airplane for emergency flight control have been conducted at the NASA Dryden Flight Research Facility. The airplane and the simulation are capable of extended up-and-away flight, using only throttles for flightpath control. Initial simulation results showed that runway landings using manual throttles only control were difficult, but possible with practice. Manual approaches flown in the airplane were much more difficult, indicating a significant discrepancy between flight and simulation. Analysis of flight data and development of improved simulation models that resolve the discrepancy are discussed. An augmented throttles-only control system that controls bank angle and flightpath with appropriate feedback parameters has also been developed, evaluated in simulations, and is planned for flight in the F-15.
Document ID
19930027281
Acquisition Source
Armstrong Flight Research Center
Document Type
Conference Paper
Authors
Frank W Burcham, Jr
(Dryden Flight Research Facility Edwards, California, United States)
Trindel Maine
(Dryden Flight Research Facility Edwards, California, United States)
Thomas Wolf
(Dryden Flight Research Facility Edwards, California, United States)
Date Acquired
August 15, 2013
Publication Date
August 24, 1992
Publication Information
Publication: 6th AIAA Biennial Flight Test Conference
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Aircraft Design, Testing and Performance
Report/Patent Number
AIAA-92-4109
Meeting Information
Meeting: 6th AIAA Biennial Flight Test Conference
Location: Hilton Head, SC
Country: US
Start Date: August 24, 1992
End Date: August 26, 1992
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
93A11278
Funding Number(s)
PROJECT: RTOP 533-02-36
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Flight Testing
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