A preliminary investigation of the use of throttles for emergency flight control
Author(s) -
Frank W. Burcham,
C. Gordon Fullerton,
Glenn B. Gilyard,
Thomas D. Wolf,
J.R. Stewart
Publication year - 1991
Publication title -
27th joint propulsion conference
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.1991-2222
Subject(s) - computer science , control (management) , automotive engineering , aeronautics , engineering , artificial intelligence
A preliminary investigation was conducted regarding the use of throttles for emergency flight control of a multiengine aircraft. Several airplanes including a light twin-engine piston-powered airplane, jet transports, and a high performance fighter were studied during flight and piloted simulations. Simulation studies used the B-720, B-727, MD-11, and F-15 aircraft. Flight studies used the Lear 24, Piper PA-30, and F-15 airplanes. Based on simulator and flight results, all the airplanes exhibited some control capability with throttles. With piloted simulators, landings using manual throttles-only control were extremely difficult. An augmented control system was developed that converts conventional pilot stick inputs into appropriate throttle commands. With the augmented system, the B-720 and F-15 simulations were evaluated and could be landed successfully. Flight and simulation data were compared for the F-15 airplane.
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