Instantaneous Wind-Tunnel Model Vibration Measurements Using a Kalman Filtering Approach
Author:
Affiliation:
1. Department of Aerospace Engineering, Texas A&M University, College Station, TX 77840 e-mail:
2. Department of Aerospace Engineering, Texas A&M University, College Station, TX 77840
3. PM & AM Research, LLC, Bryan, TX 77802
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/fluidsengineering/article-pdf/doi/10.1115/1.4036270/6199451/fe_139_07_071106.pdf
Reference12 articles.
1. Model Attitude Measurements at NASA Langley Research Center,1992
2. Model Attitude Determination in Wind Tunnel With a Luminescent Paint Data System;AIAA J.,2000
3. Wind Tunnel Experiment of Bluff Body Aerodynamic Models Using a New Type of Magnetic Suspension and Balance System;ASME J. Fluids Eng.,2013
4. Comparison of Model Attitude Systems—Active Target Photogrammetry, Precision Accelerometer, and Laser Interferometer,1996
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