APPLICATION OF KALMAN FILTERING FOR AN AEROENGINE PARAMETER ESTIMATION

Liu Xiaoyong; Fan Siqi

Volume 10 Issue 3

Jul. 1995

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Article Navigation > Journal of Aerospace Power > 1995 > 10(3): 304-306,316

Liu Xiaoyong, Fan Siqi. APPLICATION OF KALMAN FILTERING FOR AN AEROENGINE PARAMETER ESTIMATION[J]. Journal of Aerospace Power, 1995, 10(3): 304-306,316.

Citation:

Liu Xiaoyong, Fan Siqi. APPLICATION OF KALMAN FILTERING FOR AN AEROENGINE PARAMETER ESTIMATION[J]. Journal of Aerospace Power, 1995, 10(3): 304-306,316.

Liu Xiaoyong, Fan Siqi. APPLICATION OF KALMAN FILTERING FOR AN AEROENGINE PARAMETER ESTIMATION[J]. Journal of Aerospace Power, 1995, 10(3): 304-306,316.

Citation:

Liu Xiaoyong, Fan Siqi. APPLICATION OF KALMAN FILTERING FOR AN AEROENGINE PARAMETER ESTIMATION[J]. Journal of Aerospace Power, 1995, 10(3): 304-306,316.

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APPLICATION OF KALMAN FILTERING FOR AN AEROENGINE PARAMETER ESTIMATION

7th Dept.Northwestern Polytechnical University,Xi′an 710071

Received Date: 1994-09-01
Rev Recd Date: 1994-12-01
Publish Date: 1995-07-28

Abstract

Abstract

The Kalman filtering method for an aeroengine parameter estimation has been investigated by using flight data.The research purpose is to solve the Kalman filtering divergence problem in the aeroengine parameter estimation.The main content is the integrated Kalman filtering method of the adaptive processing,the compensation in flight condition and the aeroengine modification.Finally,the results of the parameter estimation are presented.