The 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.
Overview of Integrated Flight-Propulsion Controls Flight Research on the NASA F-15 Research Airplane
1995
28 pages
Report
No indication
English
Jet & Gas Turbine Engines , Avionics , Aircraft control , Digital systems , F-15 aircraft , Flight control , Flight tests , Optimal control , Research aircraft , Thrust control , Turbofan engines , Turbojet engine control , Acoustics , Bibliographies , Control surfaces , Control systems design , Electronic control , Engine inlets
NTRS | 2016
|NTIS | 2016
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