A comparison of extended Kalman filter, ultrasound time-of-flight measurement models for heating source localization-Reference-Cited by-同舟云学术

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A comparison of extended Kalman filter, ultrasound time-of-flight measurement models for heating source localization

Published:2012-04-05 Issue:7 Volume:20 Page:991-1016
ISSN:1741-5977
Container-title:Inverse Problems in Science and Engineering
language:en
Short-container-title:Inverse Problems in Science and Engineering

Author:

Myers M.R.¹,Jorge A.B.²,Mutton M.J.³,Walker D.G.¹

Affiliation:

1. Department of Mechanical Engineering, Vanderbilt University, Nashville, TN 37235, USA

2. Mechanical Engineering Institute, Federal University of Itajubá, Itajubá, MG, Brazil

3. Industrial Measurement Systems, Inc., 2760 Beverly Drive, Suite 4, Aurora, IL 60502, USA

Publisher

Informa UK Limited

Subject

Applied Mathematics,Computer Science Applications,General Engineering

Link

https://www.tandfonline.com/doi/pdf/10.1080/17415977.2012.669272

Reference31 articles.

1. Reed, HL, Kimmel, RL, Schneider, S, Arnal, D, and Saric, W, Drag Prediction and Transition in Hypersonic Flow, in Symposium on Sustained Hypersonic Flight, AGARD Conference on Future Aerospace Technology in the Service of the Alliance, Palaiseau, France, 1997.

2. Horvath, TJ, Berry, SA, and Hollis, BR, Boundary Layer Transition on Slender Cones in Conventional and Low Disturbance Mach 6 Wind Tunnels, 32nd AIAA Fluid Dynamics Conference and Exhibit, St. Louis, MO, 2002.

3. Flight Data for Boundary-Layer Transition at Hypersonic and Supersonic Speeds

4. Hypersonic laminar–turbulent transition on circular cones and scramjet forebodies

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