The Design of Aero-engine Optimal Controller Suitable for All Flight Envelope with Neural Network Approximator
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The Design of Aero-engine Optimal Controller Suitable for All Flight Envelope with Neural Network Approximator
Vol. 15, Issue 3, (2000)
作者机构:
西北工业大学航空动力与热力工程系自动控制教研室,陕西,西安,710072
作者简介:
基金信息:
DOI:
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Published:2000
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Guo Yinqing, Zhang Hong, Yang Yunbo, et al. The Design of Aero-engine Optimal Controller Suitable for All Flight Envelope with Neural Network Approximator[J]. 2000, 15(3).
DOI:
Guo Yinqing, Zhang Hong, Yang Yunbo, et al. The Design of Aero-engine Optimal Controller Suitable for All Flight Envelope with Neural Network Approximator[J]. 2000, 15(3).DOI:
The Design of Aero-engine Optimal Controller Suitable for All Flight Envelope with Neural Network Approximator
An aero engine optimal control scheme is presented
which is suitable for all points in the engine whole flight envelope with a neural network approximator.Firstly
local controllers are designed according to local linear models around some design points.Then a neural network approximator is trained to imitate the relation between the parameters of local optimal controllers and the flight conditions and the states of the engine.Finally
a global nonlinear controller is obtained with this approximator.In this approach
nonlinear control system can be designed by the use of many mature linear control methods.And the control system has simple structure
is easy of real time realization.The simulation results show that the aero engine control system has excellent characteristics in both design and non design points in whole flight envelope.