This paper presents a methodology of designing, modeling, and controlling a fully pneumatic semi-active vibration isolator system. The prototype vibration isolator system consists of an air spring, a variable orifice valve, and an accumulator which has the ability to simultaneously adjust the damping and natural frequency characteristics of the system. This paper presents a comprehensive work of modeling, hardware design, control design, and experimental validation of the proposed semi-active vibration isolation system. A higher fidelity model is obtained by complete characterization of nonlinear relationships between pressure versus volume and effective orifice area versus ride height. The performance of three semi-active controller designs — Linear Quadratic Impulse (LQI), Modified Skyhook, and Relative Displacement — is evaluated and compared experimentally using an OEM Peterbilt cabin suspension unit. The results demonstrate that the properly tuned semi-active suspension provides increased vibration isolation over the traditional passive cabin suspension design.
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ASME 2017 Dynamic Systems and Control Conference
October 11–13, 2017
Tysons, Virginia, USA
Conference Sponsors:
- Dynamic Systems and Control Division
ISBN:
978-0-7918-5829-5
PROCEEDINGS PAPER
Fully Pneumatic Semi-Active Vibration Isolator Design and Analysis
Hans W. Schaeffer,
Hans W. Schaeffer
Iowa State University, Ames, Iowa
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Atul G. Kelkar
Atul G. Kelkar
Iowa State University, Ames, Iowa
Search for other works by this author on:
Hans W. Schaeffer
Iowa State University, Ames, Iowa
Atul G. Kelkar
Iowa State University, Ames, Iowa
Paper No:
DSCC2017-5137, V003T32A005; 10 pages
Published Online:
November 14, 2017
Citation
Schaeffer, HW, & Kelkar, AG. "Fully Pneumatic Semi-Active Vibration Isolator Design and Analysis." Proceedings of the ASME 2017 Dynamic Systems and Control Conference. Volume 3: Vibration in Mechanical Systems; Modeling and Validation; Dynamic Systems and Control Education; Vibrations and Control of Systems; Modeling and Estimation for Vehicle Safety and Integrity; Modeling and Control of IC Engines and Aftertreatment Systems; Unmanned Aerial Vehicles (UAVs) and Their Applications; Dynamics and Control of Renewable Energy Systems; Energy Harvesting; Control of Smart Buildings and Microgrids; Energy Systems. Tysons, Virginia, USA. October 11–13, 2017. V003T32A005. ASME. https://doi.org/10.1115/DSCC2017-5137
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