Development and Flight Test of an Emergency Flight Control System Using Only Engine Thrust on an MD-11 Transport Airplane

Burcham Jr., Frank W. and Burken, John J. and Maine, Trindel A. and Fullerton, C. Gordon (1997) Development and Flight Test of an Emergency Flight Control System Using Only Engine Thrust on an MD-11 Transport Airplane. Technical Report NASA /TP-97-206217, Research Engineering, NASA Dryden Flight Research Center.

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Abstract

An emergency flight control system that uses only engine thrust, called the propulsion-controlled aircraft (PCA) system, was developed and flight tested on an MD-11 airplane. The PCA system is a thrust-only control system, which augments pilot flightpath and track commands with aircraft feedback parameters to control engine thrust. The PCA system was implemented on the MD-11 airplane using only software modifications to existing computers. Results of a 25-hr flight test show that the PCA system can be used to fly to an airport and safely land a transport airplane with an inoperative flight control system. In up-and-away operation, the PCA system served as an acceptable autopilot capable of extended flight over a range of speeds, altitudes, and configurations. PCA approaches, go-arounds, and three landings without the use of any normal flight controls were demonstrated, including ILS-coupled hands-off landings. PCA operation was used to recover from an upset condition. The PCA system was also tested at altitude with all three hydraulic systems turned off. This paper reviews the principles of throttles-only flight control, a history of accidents or incidents in which some or all flight controls were lost, the MD-11 airplane and its systems, PCA system development, operation, flight testing, and pilot comments.

EPrint Type:	NASA Technical Publication
Keywords:	Emergency Control, MD-11, Propulsion Control, Throttle-only control
Subjects:	Aircraft/Project: MD-11 (01 - 09) Aeronautics: (08) Aircraft Stability And Control
ID Code:	148
Deposited On:	08 June 2004
Additional Information:	98 pages.