Skip Nav Destination
Close Modal
Update search
Filter
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- ISBN-10
- ISSN
- EISSN
- Issue
- Journal Volume Number
- References
- Conference Volume Title
- Paper No
Filter
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- ISBN-10
- ISSN
- EISSN
- Issue
- Journal Volume Number
- References
- Conference Volume Title
- Paper No
Filter
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- ISBN-10
- ISSN
- EISSN
- Issue
- Journal Volume Number
- References
- Conference Volume Title
- Paper No
Filter
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- ISBN-10
- ISSN
- EISSN
- Issue
- Journal Volume Number
- References
- Conference Volume Title
- Paper No
Filter
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- ISBN-10
- ISSN
- EISSN
- Issue
- Journal Volume Number
- References
- Conference Volume Title
- Paper No
Filter
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- ISBN-10
- ISSN
- EISSN
- Issue
- Journal Volume Number
- References
- Conference Volume Title
- Paper No
NARROW
Format
Article Type
Subject Area
Topics
Date
Availability
1-5 of 5
Keywords: aircraft control
Close
Follow your search
Access your saved searches in your account
Would you like to receive an alert when new items match your search?
Sort by
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Eng. Gas Turbines Power. April 2012, 134(4): 041601.
Published Online: January 27, 2012
... methodology is shown to yield a significant improvement in on-line Kalman filter estimation accuracy. 25 04 2011 28 04 2011 27 01 2012 27 01 2012 aerospace engines aircraft control closed loop systems dynamic response Kalman filters mean square error methods open loop systems...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Eng. Gas Turbines Power. January 2012, 134(1): 011603.
Published Online: November 7, 2011
... Margin Control Mode ,” ASME J. Eng. Gas Turbines Power , 132 ( 5 ), p. 051602 . 25 04 2011 03 05 2011 07 11 2011 07 11 2011 aircraft control compressors correlation methods gas turbines rotors stability The control systems for aircraft gas turbine engines...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Eng. Gas Turbines Power. November 2011, 133(11): 111601.
Published Online: May 17, 2011
... the nonlinear control issues based on this model. Control validations are provided in Sec. 5 . Finally the paper is summarized in Sec. 6 . 01 07 2010 30 01 2011 17 05 2011 17 05 2011 aerospace engines aircraft control closed loop systems feedback jet engines...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Eng. Gas Turbines Power. May 2010, 132(5): 051602.
Published Online: March 4, 2010
... , Austin, TX, Paper No. AIAA-2003-5425. 25 03 2009 09 04 2009 04 03 2010 04 03 2010 aerospace engines aircraft control compressors gas turbines stability The control system for gas turbine engines used on modern, commercial aircraft consists of a controller...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Eng. Gas Turbines Power. May 2009, 131(3): 031702.
Published Online: February 10, 2009
... due to the transient fuel flow change using the Runge–Kutta method. In this transient performance simulation, the turbine overshoot was predicted. 31 03 2008 09 04 2008 10 02 2009 aerospace computing aerospace engines aerospace propulsion aircraft control control engineering...
