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Variable cycle engine intelligent control method based on dynamic neural network

A dynamic neural network, variable cycle engine technology, applied in engine control, machine/engine, mechanical equipment, etc., can solve the problems of model accuracy affecting the controller, slow training, overfitting, etc.

Active Publication Date: 2020-04-21
DALIAN UNIV OF TECH
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  • Summary
  • Abstract
  • Description
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  • Application Information

AI Technical Summary

Problems solved by technology

Most of the existing control methods are based on accurate engine models, which will cause the accuracy of the model to directly affect the control effect of the controller, and cannot solve the coupling problem between nonlinear variables well.
Due to the nonlinear characteristics of the neural network itself, the controller based on the neural network can well solve the coupling problem between multiple variables, but during training, it is impossible to directly determine the structure of the hidden layer. If the structure is too large, the training will be too slow and Overfitting; the required accuracy cannot be achieved if the structure is too small

Method used

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  • Variable cycle engine intelligent control method based on dynamic neural network
  • Variable cycle engine intelligent control method based on dynamic neural network
  • Variable cycle engine intelligent control method based on dynamic neural network

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Embodiment Construction

[0063] The examples of the present invention will be described in detail below in conjunction with the accompanying drawings and technical solutions.

[0064] Concrete steps of the present invention are as follows:

[0065] Step 1: Construct the training sample set of the dynamic neural network.

[0066] Step 1.1: Take 0.01s as the sampling period to collect the operating parameters of the variable cycle engine at a specific height and throttle lever angle. Including the controlled variable high pressure relative speed n h The actual value and expected value of , the expected value and actual value of the pressure ratio π and the control variable: fuel flow W f , the critical area of ​​the tail nozzle A 8 , High pressure turbine guide area A HTG , Fan guide vane angle α f , core engine fan guide vane angle α CDFS , Compressor guide vane angle α c , High pressure compressor guide vane angle α turb , core machine fan mixer area A CDFS actual operating value.

[0067] S...

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Abstract

The invention belongs to the technical field of aero-engine control and provides a variable cycle engine intelligent control method based on a dynamic neural network. A structure adjustment algorithmbased on a grey correlation analysis method is added into a neural network training algorithm, a neural network structure is adjusted, a dynamic neural network controller is constructed, and intelligent control of a variable-cycle engine is achieved. Dynamic neural network training is performed through a network structure adjustment algorithm based on the grey correlation analysis method designedin the invention, and a variable cycle engine dynamic intelligent controller based on the dynamic neural network is constructed. A coupling problem between nonlinear multivariables caused by increaseof control variables of the variable cycle engine and the problem that a traditional control method excessively depends on model precision are effectively solved. And meanwhile, the structure can be dynamically adjusted in a neural network training process so that the network structure is simpler, and an operation speed and the control precision are improved.

Description

technical field [0001] The invention belongs to the technical field of aero-engine control, and in particular relates to an intelligent control method of a variable-cycle engine based on a dynamic neural network. Background technique [0002] The control system is an important part of an aero-engine and a key factor affecting the performance of an aero-engine. The variable cycle engine combines the advantages of turbojet and turbofan engines, and adds geometrically adjustable components. By adaptively adjusting the geometric shape, position and other parameters of these components, the variable cycle engine can have high unit thrust in the aircraft maneuvering phases such as acceleration and climb; it can have low fuel consumption in the subsonic cruising phase. However, due to the increase of adjustable components, the number of control variables increases, and the structure of the controller is more complex; at the same time, there is a strong coupling relationship betwee...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02C9/00
CPCF02C9/00F05D2270/709
Inventor 王甜马艳华杜宪夏卫国孙希明
Owner DALIAN UNIV OF TECH
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