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Integrated Flight/Propulsion Control System Considerations for Future Aircraft Application
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Flight and propulsion controls can effectively be integrated to provide operational benefits to the weapon system which cannot be achieved with either system acting independently. The key factor ...
Engine Control Reliability and Durability Improvement Through Accelerated Mission Environmental Testing
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The integration of aircraft control systems for future weapon systems will require the engine control system to meet the mission reliability of the flight control system. This will be accomplished ...
F-14 Aircraft and Propulsion Control Integration Evaluation
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Since 1976, the U.S. Navy in conjunction with Pratt and Whitney Aircraft (PWA) has been actively engaged in developing the technology base for on engine, dual redundant, fault tolerant, full ...
Conceptual Design of an Optic-Based Engine Control System
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Advanced integrated flight and propulsion control systems may require the use of optic technology to provide enhanced electromagnetic immunity and reduced weight. Immunity to electromagnetic ...