Integrated Flight Propulsion Control Research Results Using the NASA F-15 HIDEC Flight Research Facility

Stewart, James F. (1992) Integrated Flight Propulsion Control Research Results Using the NASA F-15 HIDEC Flight Research Facility. Technical Report NASA TM-4394, Research Engineering, NASA Dryden Flight Research Center.

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Abstract

Over the last two decades, NASA has conducted several flight research experiments in integrated flight-propulsion control. Benefits have included increased thrust, range, and survivability; reduced fuel consumption; and reduced maintenance. The flight programs were flown at NASA Dryden Flight Research Facility. This paper presents the basic concepts for control integration, examples of implementation, and benefits of integrated flight propulsion control systems. The F-15 research involved integration of the engine, flight, and inlet control systems. Further extension of the integration included real-time, onboard optimization of engine, inlet, and flight control variables; a self-repairing flight control system; and an engines-only control concept for emergency control. The flight research programs and the resulting benefits are described for the F-15 research.

EPrint Type:	NASA Technical Memorandum
Keywords:	F-15 HIDEC, Integrated flight propulsion control, Performance seeking control
Subjects:	Aircraft/Project: F-15 HIDEC (01 - 09) Aeronautics: (07) Aircraft Propulsion And Power
ID Code:	285
Deposited On:	27 July 2004
Additional Information:	22 pages. Prepared as AIAA paper 92-4106 for the 6th Biannual Flight Test Conference, Hilton Head, SC, August 24–26, 1992.