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Preview Control of a Semi-Active Suspension System Supplemented by an Active Aerodynamic Surfaceopen access

Authors
Abbas, Syed BabarYoun, Iljoong
Issue Date
Nov-2025
Publisher
Multidisciplinary Digital Publishing Institute (MDPI)
Keywords
passengerride comfort; optimal preview control; aerodynamic control surface; semi-active suspension system
Citation
Sensors, v.25, no.22
Indexed
SCIE
SCOPUS
Journal Title
Sensors
Volume
25
Number
22
URI
https://scholarworks.gnu.ac.kr/handle/sw.gnu/81340
DOI
10.3390/s25226922
ISSN
1424-8220
1424-8220
Abstract
This research presents a harmonized optimal preview control strategy for a semi-active suspension system (SASS) with a controlled damper varied between the upper and lower bounds of the damping coefficient and an active aerodynamic surface (AAS) control. The preview control algorithm is based on a simplified bilinear 2-DOF quarter-car model to address the tradeoff between passenger ride comfort and road holding capabilities. While the active suspension with the actuator requires a significant amount of energy to provide control force, the semi-active suspension system with a variable damping coefficient mechanism consumes minimal energy to adapt quickly to the real-time operating conditions. Moreover, the dynamic performance of semi-active suspension with the preview controller in conjunction with the active aerodynamic surface is significantly improved. MATLAB (R) (R2025b)-based numerical simulations for different road excitations were carried out for the evaluation of the proposed system. Both time-domain and frequency-domain results demonstrate enhanced vehicle dynamic performances in response to road bumps, asphalt road excitations, and harmonic input signals. The simulation performance results indicate that the proposed system extraordinarily reduced the variation in the mean-squared value of the car body vertical acceleration. At the same time, the system enhanced the wheel-road holding metric by decreasing the variation in the gripping force on the ground surface, while maintaining the necessary suspension rattle space constraints within the prescribed limit.
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공학계열 > 기계항공우주공학부 > Journal Articles

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Youn, Il Joong
대학원 (기계항공우주공학부)
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