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Development of HIDEC adaptive engine control systemsThe purpose of NASA's Highly Integrated Digital Electronic Control (HIDEC) flight research program is the development of integrated flight propulsion control modes, and the evaluation of their benefits aboard an F-15 test aircraft. HIDEC program phases are discussed, with attention to the Adaptive Engine Control System (ADECS I); this involves the upgrading of PW1128 engines for operation at higher engine pressure ratios and the production of greater thrust. ADECS II will involve the development of a constant thrust mode which will significantly reduce turbine operating temperatures.
Document ID
19860063540
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Landy, R. J.
(McDonnell Aircraft Co. Saint Louis, MO, United States)
Yonke, W. A.
(McDonnell Aircraft Co. Saint Louis, MO, United States)
Stewart, J. F.
(NASA Flight Research Center Edwards, CA, United States)
Date Acquired
August 12, 2013
Publication Date
June 1, 1986
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
ASME PAPER 86-GT-252
Accession Number
86A48278
Distribution Limits
Public
Copyright
Other

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