Model-Based Control of a Nonlinear Aircraft Engine Simulation using an Optimal Tuner Kalman Filter Approach-Reference-Cited by-同舟云学术

Model-Based Control of a Nonlinear Aircraft Engine Simulation using an Optimal Tuner Kalman Filter Approach

Published:2013-07-12 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
language:
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Author:

Connolly Joseph W.¹,Csank Jeffrey¹,Chicatelli Amy²,Kilver Jacob³

Affiliation:

1. NASA Glenn Research Center

2. Vantage Partners, LLC

3. Ohio State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-4002

Reference18 articles.

1. 1“NASA Fact Sheet: Energy, Efficiency and Emissions.” Tech. Rep. NASA/NF-2009-08-488-HQ, NASA, 2009.

2. 2May, R., Csank, J., Litt, J. S., and Guo, T. “Commercial Modular Aero-Propulsion System Simulation 40K,” Tech. Rep. NASA/TM 2010-216810, NASA, 2009.

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