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An overview of integrated flight-propulsion controls flight research on the NASA F-15 research airplaneThe NASA Dryden Flight Research Center has been conducting integrated flight-propulsion control flight research using the NASA F-15 airplane for the past 12 years. The research began with the digital electronic engine control (DEEC) project, followed by the F100 Engine Model Derivative (EMD). HIDEC (Highly Integrated Digital Electronic Control) became the umbrella name for a series of experiments including: the Advanced Digital Engine Controls System (ADECS), a twin jet acoustics flight experiment, self-repairing flight control system (SRFCS), performance-seeking control (PSC), and propulsion controlled aircraft (PCA). The upcoming F-15 project is ACTIVE (Advanced Control Technology for Integrated Vehicles). This paper provides a brief summary of these activities and provides background for the PCA and PSC papers, and includes a bibliography of all papers and reports from the NASA F-15 project.
Document ID
19950026589
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Burcham, Frank W., Jr.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Gatlin, Donald H.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Stewart, James F.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1995
Publication Information
Publication: An Electronic Workshop on the Performance Seeking Control and Propulsion Controlled Aircraft Results of the F-15 Highly Integrated Digital Electronic Control Flight Research Program
Subject Category
Aircraft Propulsion And Power
Accession Number
95N33010
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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