System and method for active aerodynamic device control for a vehicle

    公开(公告)号:US11548498B2

    公开(公告)日:2023-01-10

    申请号:US16792538

    申请日:2020-02-17

    IPC分类号: B60W30/02 B60W40/08

    摘要: A dynamic vehicle stability control system for a vehicle may include an active wing extending laterally relative to a longitudinal centerline of the vehicle and configured to be rotatable to change an angle of attack relative to wind passing over the vehicle parallel to the longitudinal centerline, a repositioning assembly operably coupling the active wing to the vehicle, and a controller operably coupled to components and/or a sensor network of the vehicle to receive status information about the vehicle. The repositioning assembly may be operated based on a wing angle command received by the controller responsive to execution of a plurality of control algorithms executed by the controller. The controller may be configured to determine the wing angle command based on respective wing angle requests generated by each of the control algorithms.

    SYSTEM AND METHOD FOR ACTIVE AERODYNAMIC DEVICE CONTROL FOR A VEHICLE

    公开(公告)号:US20210253087A1

    公开(公告)日:2021-08-19

    申请号:US16792538

    申请日:2020-02-17

    IPC分类号: B60W30/02 B60W40/08

    摘要: A dynamic vehicle stability control system for a vehicle may include an active wing extending laterally relative to a longitudinal centerline of the vehicle and configured to be rotatable to change an angle of attack relative to wind passing over the vehicle parallel to the longitudinal centerline, a repositioning assembly operably coupling the active wing to the vehicle, and a controller operably coupled to components and/or a sensor network of the vehicle to receive status information about the vehicle. The repositioning assembly may be operated based on a wing angle command received by the controller responsive to execution of a plurality of control algorithms executed by the controller. The controller may be configured to determine the wing angle command based on respective wing angle requests generated by each of the control algorithms.