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STOVL Control Integration ProgramAn integrated flight/propulsion control for an advanced vector thrust supersonic STOVL aircraft, was developed by Pratt & Whitney and McDonnell Douglas Aerospace East. The IFPC design was based upon the partitioning of the global requirements into flight control and propulsion control requirements. To validate the design, aircraft and engine models were also developed for use on a NASA Ames piloted simulator. Different flight control implementations, evaluated for their handling qualities, are documented in the report along with the propulsion control, engine model, and aircraft model.
Document ID
19950005074
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Weiss, C.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Mcdowell, P.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Watts, S.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1994
Publication Information
Publisher: NASA
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.26:195358
E-9023
NASA-CR-195358
Report Number: NAS 1.26:195358
Report Number: E-9023
Report Number: NASA-CR-195358
Accession Number
95N11487
Funding Number(s)
PROJECT: RTOP 505-68-32
CONTRACT_GRANT: NAS3-25194
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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