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High Stability Engine Control (HISTEC) Flight Test ResultsThe High Stability Engine Control (HISTEC) Program, managed and funded by the NASA Lewis Research Center, is a cooperative effort between NASA and Pratt & Whitney (P&W). The program objective is to develop and flight demonstrate an advanced high stability integrated engine control system that uses real-time, measurement-based estimation of inlet pressure distortion to enhance engine stability. Flight testing was performed using the NASA Advanced Controls Technologies for Integrated Vehicles (ACTIVE) F-15 aircraft at the NASA Dryden Flight Research Center. The flight test configuration, details of the research objectives, and the flight test matrix to achieve those objectives are presented. Flight test results are discussed that show the design approach can accurately estimate distortion and perform real-time control actions for engine accommodation.
Document ID
19980211493
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Southwick, Robert D.
(Pratt and Whitney Aircraft West Palm Beach, FL United States)
Gallops, George W.
(Pratt and Whitney Aircraft West Palm Beach, FL United States)
Kerr, Laura J.
(Pratt and Whitney Aircraft West Palm Beach, FL United States)
Kielb, Robert P.
(Pratt and Whitney Aircraft West Palm Beach, FL United States)
Welsh, Mark G.
(Pratt and Whitney Aircraft West Palm Beach, FL United States)
DeLaat, John C.
(NASA Lewis Research Center Cleveland, OH United States)
Orme, John S.
(NASA Dryden Flight Research Center Edwards, CA United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1998
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA/TM-1998-208481
AIAA Paper 98-3757
E-11255
NAS 1.15:208481
Report Number: NASA/TM-1998-208481
Report Number: AIAA Paper 98-3757
Report Number: E-11255
Report Number: NAS 1.15:208481
Meeting Information
Meeting: Propulsion
Location: Cleveland, OH
Country: United States
Start Date: July 12, 1998
End Date: July 15, 1998
Sponsors: American Society of Mechanical Engineers, American Inst. of Aeronautics and Astronautics, Society of Automotive Engineers, Inc., American Society for Electrical Engineers
Funding Number(s)
PROJECT: RTOP 523-53-13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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