“…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.…”