Index RECONselect contains the following 61 items relevant to 'FADEC'. The first figure for each entry is its relative score,

• 1000 -1 Full authority digital electronic control /FADEC/ - Variable cycle engine demonstration, AIAA PAPER 81-1498, Jul 01, 1981

• 982 -1 Potential benefits of a Full Authority Digital Electronic Control (FADEC) installed on a TF30 engine in an F14 flight test demonstrator aircraft, Feb 01, 1983

• 818 -1 FADEC - Every jet engine should have one, SAE PAPER 861802, Oct 01, 1986

• 817 -1 FADEC for fighter engines, Nov 01, 1986

• 785 -1 Full Authority Digital Electronic Control (FADEC) - Augmented fighter engine demonstration, SAE PAPER 821371, Oct 01, 1982

• 597 -1 Using a personal computer as a Full Authority Digital Electronic Control Interface System for gas turbine testing, Jan 01, 1992

• 587 -1 Digital engine control for V/STOL and V/TOL aircraft, Sep 01, 1982

• 573 -1 FADEC - Digital propulsion control of the future, AIAA PAPER 76-652, Jul 01, 1976

• 530 -1 Full authority digital electronic control turbofan engine demonstration, Mar 01, 1981

• 529 -1 Certification of lightning protection for a full-authority digital engine control, Aug 01, 1991

• 477 -1 Chinook goes FADEC, CONGRESS PAPER C428-33-078, Jan 01, 1991

• 457 -1 Future engine controls, Jan 01, 1988

• 454 -1 Full authority digital electronic control /FADEC/ preliminary design overview for a variable cycle engine, AIAA PAPER 77-837, Jul 01, 1977

• 441 -1 Developments towards versatility in digital engine control units, ISABE 93-7088, Jan 01, 1993

• 440 -1 Real-time simulation and adaptive PID control of QSK-06A control for gas turbine, Jan 01, 1991

• 440 -1 Integrated propulsion-aircraft control evaluation for a current Navy fighter, AIAA PAPER 83-1236, Jun 01, 1983

• 357 -1 F-14 aircraft and propulsion control integration evaluation, ASME PAPER 83-GT-234, Mar 01, 1983

• 350 -1 Advanced propulsion controls - A total system view, May 01, 1983

• 348 -1 Engine controls for the 1980s and 1990s, Jan 01, 1982

• 346 -1 Enhanced fighter engine operability using full authority digital electronic control systems, AIAA PAPER 88-3266, Jul 01, 1988

• 344 -1 Full-authority digital electronic controls for civil aircraft engines, ASME PAPER 81-GT-139, Mar 01, 1981

• 342 -1 Pusher turboprop installation technology for the Embraer CBA-123 vector, SAE PAPER 911030, Apr 01, 1991

• 341 -1 Upgraded T55 engine for Special Forces MH-47E aircraft, AIAA PAPER 91-2024, Jun 01, 1991

• 341 -1 Single lever power management of turboprop engines, SAE PAPER 912200, Sep 01, 1991

• 338 -1 Digital controls for gas turbine engines, ASME PAPER 87-GT-211, May 01, 1987

• 337 -1 Energy Efficient Engine: Control system component performance report, NASA-CR-174651, Oct 01, 1984

• 332 -1 Real time simulators for use in design of integrated flight and propulsion control systems, ASME PAPER 88-GT-24, Jun 01, 1988

• 330 -1 Full Authority Digital Engine Control for the AS 355 N TM 319 engines, Sep 01, 1988

• 322 -1 Review of Photonic System Development for Propulsion Controls, Jun 01, 1996

• 321 -1 Full Authority Digital Electronic Control turbofan engine demonstration, SAE PAPER 801199, Oct 01, 1980

• 320 -1 Distributed Architectures for Advanced Engine Control Systems, Jun 01, 1996

• 317 -1 Lightning protection of full authority digital electronic systems, Aug 01, 1991

• 237 -1 An aircraft controller and its development, Jan 01, 1992

• 229 -1 Assessment of augmented electronic fuel controls for modular engine diagnostics and condition monitoring, AD-A065128, Dec 01, 1978

• 228 -1 The PW2000 - A mature engine with an eye to the future, SAE PAPER 892365, Sep 01, 1989

• 227 -1 Airworthiness considerations of lightning strike protection for helicopter digital engine controls, Jan 01, 1986

• 227 -1 New functional requirement to aero-engine control system, Jan 01, 1984

• 225 -1 Development of digital electronic control for aeroengine, Sep 01, 1987

• 224 -1 Software methodologies for safety critical systems, Sep 01, 1991

• 223 -1 An appraisal of a number of power assessment procedures being proposed for use in Chinook-Lycoming T55 engine, AD-A210482, Feb 01, 1989

• 223 -1 The role of avionics in the all electric airplane, AIAA PAPER 81-2219, Jan 01, 1981

• 221 -1 Optical sensors and multiplexing for aircraft engine control, Jan 01, 1993

• 221 -1 Simplified mathematical model and digital simulation of aeroengine, Apr 01, 1993

• 220 -1 Advanced Control System for a Turbine Engine, Jun 01, 1996

• 220 -1 Research and development of turbofan engine for supersonic aircraft, Jan 01, 1992

• 220 -1 Overview of the Japanese National Project for Super/Hyper-Sonic Transport propulsion system, ASME PAPER 92-GT-252, Jun 01, 1992

• 219 -1 Reliability and safety considerations in engine management systems design, Jan 01, 1991

• 217 -1 Failure detection of engine sensors with a bank of Kalman filters, Jan 01, 1992

• 217 -1 Full authority digital electronic control application to a variable cycle engine, SAE PAPER 801203, Oct 01, 1980

• 216 -1 Optical temperature compensation schemes of spectral modulation sensors for aircraft engine control, Jan 01, 1993

• 216 -1 Advanced developments of the Turbo-Union RB199, Dec 01, 1989

• 215 -1 The application of Ada and formal methods to a safety critical engine control system, Mar 01, 1995

• 213 -1 Automatic throttle control for business and commuter aircraft, Jan 01, 1990

• 212 -1 Full Authority Fault Tolerant Electronic Engine Control systems for advanced high performance engines (FAFTEEC), SAE PAPER 821398, Oct 01, 1982

• 212 -1 Modernizing engine displays, Jan 01, 1984, DFRC

• 211 -1 Flight testing of the Chandler Evans adaptive fuel control on the S-76A helicopter, Jan 01, 1989

• 208 -1 Design of lightning protection for a full-authority digital engine control, Aug 01, 1991

• 207 -1 Model-Based Diagnostics of Gas Turbine Engine Lubrication Systems, AD-A347307, Jan 01, 1998

• 204 -1 Hot gas ingestion effects on fuel control surge recovery and AH-1 rotor drive train torque spikes, AD-A290130, Apr 01, 1994

• 197 -1 PW2037 starts work, Nov 10, 1984

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