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HIDEC F-15 adaptive engine control system flight test resultsNASA-Ames' Highly Integrated Digital Electronic Control (HIDEC) flight test program aims to develop fully integrated airframe, propulsion, and flight control systems. The HIDEC F-15 adaptive engine control system flight test program has demonstrated that significant performance improvements are obtainable through the retention of stall-free engine operation throughout the aircraft flight and maneuver envelopes. The greatest thrust increase was projected for the medium-to-high altitude flight regime at subsonic speed which is of such importance to air combat. Adaptive engine control systems such as the HIDEC F-15's can be used to upgrade the performance of existing aircraft without resort to expensive reengining programs.
Document ID
19880064206
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Smolka, James W.
(NASA Flight Research Center Edwards, CA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Aircraft Propulsion And Power
Accession Number
88A51433
Distribution Limits
Public
Copyright
Other

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