Adaptive Optimization of Aircraft Engine Performance Using Neural Networks

Preliminary results are presented on the development of an adaptive neural network based control algorithm to enhance aircraft engine performance. This work builds upon a previous National Aeronautics and Space Administration (NASA) effort known as Performance Seeking Control (PSC). PSC is an adapti...

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description Preliminary results are presented on the development of an adaptive neural network based control algorithm to enhance aircraft engine performance. This work builds upon a previous National Aeronautics and Space Administration (NASA) effort known as Performance Seeking Control (PSC). PSC is an adaptive control algorithm which contains a model of the aircraft's propulsion system which is updated on-line to match the operation of the aircraft's actual propulsion system. Information from the on-line model is used to adapt the control system during flight to allow optimal operation of the aircraft's propulsion system (inlet, engine, and nozzle) to improve aircraft engine performance without compromising reliability or operability. Performance Seeking Control has been shown to yield reductions in fuel flow, increases in thrust, and reductions in engine fan turbine inlet temperature. The neural network based adaptive control, like PSC, will contain a model of the propulsion system which will be used to calculate optimal control commands on-line. Hopes are that it will be able to provide some additional benefits above and beyond those of PSC. The PSC algorithm is computationally intensive, it is valid only at near steady-state flight conditions, and it has no way to adapt or learn on-line. These increases are being addressed in the development of the optimal neural controller. Specialized neural network processing hardware is being developed to run the software, the algorithm will be valid at steady-state and transient conditions, and will take advantage of the on-line learning capability of neural networks. Future plans include testing the neural network software and hardware prototype against an aircraft engine simulation. In this paper the proposed neural network software and hardware is described and preliminary neural network training results are presented. Presented at the Symposium on Advanced Aero Engines Concepts and Controls, Bellevue, WA 25-29 Sep 95. Prepared in collaboration with NeuroDyne, Inc. Williamsburg, VA.
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This work builds upon a previous National Aeronautics and Space Administration (NASA) effort known as Performance Seeking Control (PSC). PSC is an adaptive control algorithm which contains a model of the aircraft's propulsion system which is updated on-line to match the operation of the aircraft's actual propulsion system. Information from the on-line model is used to adapt the control system during flight to allow optimal operation of the aircraft's propulsion system (inlet, engine, and nozzle) to improve aircraft engine performance without compromising reliability or operability. Performance Seeking Control has been shown to yield reductions in fuel flow, increases in thrust, and reductions in engine fan turbine inlet temperature. The neural network based adaptive control, like PSC, will contain a model of the propulsion system which will be used to calculate optimal control commands on-line. Hopes are that it will be able to provide some additional benefits above and beyond those of PSC. The PSC algorithm is computationally intensive, it is valid only at near steady-state flight conditions, and it has no way to adapt or learn on-line. These increases are being addressed in the development of the optimal neural controller. Specialized neural network processing hardware is being developed to run the software, the algorithm will be valid at steady-state and transient conditions, and will take advantage of the on-line learning capability of neural networks. Future plans include testing the neural network software and hardware prototype against an aircraft engine simulation. In this paper the proposed neural network software and hardware is described and preliminary neural network training results are presented. Presented at the Symposium on Advanced Aero Engines Concepts and Controls, Bellevue, WA 25-29 Sep 95. Prepared in collaboration with NeuroDyne, Inc. 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source DTIC Technical Reports
subjects ADAPTIVE CONTROL SYSTEMS
ADAPTIVE SYSTEMS
AIRCRAFT ENGINES
ALGORITHMS
COMPUTER PROGRAMS
CONTROL SYSTEMS
Cybernetics
HOMING
Jet and Gas Turbine Engines
LEARNING
NERVOUS SYSTEM
NEURAL NETS
ONLINE SYSTEMS
OPERATION
OPTIMIZATION
PERFORMANCE(ENGINEERING)
PROCESSING EQUIPMENT
PROPULSION SYSTEMS
PROTOTYPES
REDUCTION
RELIABILITY
SIMULATION
STEADY STATE
TRAINING
TRANSIENTS
TURBOFAN ENGINES
WU-244-02-01
YIELD
title Adaptive Optimization of Aircraft Engine Performance Using Neural Networks
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