An Onboard Aeroengine Model-Tuning System-Reference-Cited by-同舟云学术

An Onboard Aeroengine Model-Tuning System

Published:2017-07 Issue:4 Volume:30 Page:04017018
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Ding Shuiting¹,Yuan Ye²,Xue Naiyu³,Liu Xiaofeng⁴

Affiliation:

1. Professor, School of Energy and Power Engineering, Beihang Univ., Beijing 100191, China.

2. Ph.D. Candidate, School of Energy and Power Engineering, Beihang Univ., Beijing 100191, China.

3. Ph.D. Candidate, School of Transportation Science and Engineering, Beihang Univ., Beijing 100191, China.

4. Lecturer, School of Transportation Science and Engineering, Beihang Univ., Beijing 100191, China (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000726

Reference28 articles.

1. Armstrong J. B. and Simon D. L. (2011). “Implementation of an integrated on-board aircraft engine diagnostic architecture.” Proc. 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conf. and Exhibit American Institute of Aeronautics and Astronautics Reston VA.

2. Armstrong J. B. and Simon D. L. (2012). “Constructing an efficient self-tuning aircraft engine model for control and health management applications.” Technical Rep. NASA/TM-2012-217806 NASA Cleveland.

3. Identification of process and measurement noise covariance for state and parameter estimation using extended Kalman filter

4. Behbahani A. Adibhatla S. and Rauche C. (2009). “Integrated model-based controls and phm for improving turbine engine performance reliability and cost.” Proc. 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conf. and Exhibit American Institute of Aeronautics and Astronautics Reston VA.

5. The explicit linear quadratic regulator for constrained systems

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