2001 IEEE/ASME International Conference on Advanced Intelligent Mechatronics. Proceedings (Cat. No.01TH8556)
DOI: 10.1109/aim.2001.936476
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Analysis and control of vehicle dynamics under crosswind conditions

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Cited by 8 publications
(5 citation statements)
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“…Finally, a disturbance due to the wind is considered, which has been implemented in [2,4]. e wind induces longitudinal/lateral forces F d,x , F d,y , and a yaw moment M d,z [34]. In terms of the front/lateral surfaces A s,f , A s,l of the vehicle, the air density ρ, and the (dimensionless) front/ lateral aerodynamic coefficients c a,x , c a,y , the expression of the forces, and yaw torque due to the wind are F d,x � − (A s,f ρc a,x v 2 aw,x /2), F d,y � − (A s,l ρc a,y v 2 aw,y /2), M d,z � l c F d,y , where l c � l c0 + 0.025N is the distance between the center of mass and the center of pressure, with l c0 the nominal value and N a white noise.…”
Section: Simulation Resultsmentioning
confidence: 99%
“…Finally, a disturbance due to the wind is considered, which has been implemented in [2,4]. e wind induces longitudinal/lateral forces F d,x , F d,y , and a yaw moment M d,z [34]. In terms of the front/lateral surfaces A s,f , A s,l of the vehicle, the air density ρ, and the (dimensionless) front/ lateral aerodynamic coefficients c a,x , c a,y , the expression of the forces, and yaw torque due to the wind are F d,x � − (A s,f ρc a,x v 2 aw,x /2), F d,y � − (A s,l ρc a,y v 2 aw,y /2), M d,z � l c F d,y , where l c � l c0 + 0.025N is the distance between the center of mass and the center of pressure, with l c0 the nominal value and N a white noise.…”
Section: Simulation Resultsmentioning
confidence: 99%
“…The nominal parameters are the following The crosswind induces a pitching moment, around the y direction, a roll moment in the x direction, and a yaw moment d [5], [7], [12]. In terms of the front surface of the vehicle As = 2.5 m 2 , the overall length l f +lr of the vehicle, the air density ρ = 1.2 kg/m 3 , and the aerodynamic coefficient c ψ = 0.3, the expression of the disturbance d is d = As(l f + lr)ρc ψ v 2 w /2.…”
Section: Simulation Resultsmentioning
confidence: 99%
“…Hence, the controller (6), (7) can not be directly implemented. The signals usually measured are the longitudinal and lateral accelerations ax, ay, the angular velocity ωz and the longitudinal velocity vx of the vehicle.…”
Section: B a Simple Kinematic State Observermentioning
confidence: 98%
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