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Article type: Research Article
Authors: Fitz-Coy, Norman
Affiliations: Department of Aerospace Engineering, Mechanics, and Engineering Science, University of Florida, Gainesville, FL 32611-6250
Abstract: A mathematical procedure that quantitatively addresses issues critical to the design and operation of multiaxis vibration simulators is presented. Both kinematic and dynamic issues are considered. The analysis is applied to both 3 and 6 degrees of freedom configurations. The existence of singular configurations is mentioned and appropriate corrective measures are recommended. A methodology for determining the required actuator commands is also presented.
DOI: 10.3233/SAV-1995-2605
Journal: Shock and Vibration, vol. 2, no. 6, pp. 461-470, 1995
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