Publisher
American Institute of Aeronautics and Astronautics
Cited by
5 articles.
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1. Characterization of Root-Mean-Square Acceleration Errors in Flexible Structures Undergoing Vibration Testing;Procedia Engineering;2016
2. Optimal Force Inputs for Environmental Vibration Testing of Full Scale Slender Aerospace Vehicles;Journal of Vibration and Acoustics;2015-10-01
3. Identification of Multiple Input Forces in Vibration Testing of Flight Vehicle Structures;51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 18th AIAA/ASME/AHS Adaptive Structures Conference<BR> 12th;2010-04-12
4. Time Domain Identification of Input Forces in Vibration Testing of Flight Vehicle Structures;50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2009-05-04
5. Evolution of Vibration Testing Strategy Using Multi-Point Excitation;49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference <br> 16th AIAA/ASME/AHS Adaptive Structures Conference<br> 10t;2008-04-07