Advanced Generalized Predictive Control
    6.
    发明公开

    公开(公告)号:US20240182157A1

    公开(公告)日:2024-06-06

    申请号:US18526067

    申请日:2023-12-01

    发明人: Thomas G. Ivanco

    IPC分类号: B64C13/16

    CPC分类号: B64C13/16

    摘要: A method of controlling a vehicle utilizing a controller having a vehicle model that corresponds to the vehicle. The method includes utilizing the controller to provide inputs during vehicle operation, and measuring vehicle outputs for a plurality of times while the vehicle is in operation. The method further includes determining modeling parameters of the vehicle model to thereby model vehicle behavior, wherein the modeling parameters are determined based upon the utilized inputs and the measured outputs. Predicted vehicle outputs for the plurality of times are determined, at least in part, by utilizing the determined modeling parameters. The system further includes determining a system error for the plurality of times utilizing a difference between the measured vehicle outputs and the predicted vehicle outputs. The vehicle model is modified to provide adaptive changes while the vehicle is in operation based, at least in part, on the system error.

    Rapid aero modeling for computational experiments (RAM-C)

    公开(公告)号:US11983467B2

    公开(公告)日:2024-05-14

    申请号:US17144995

    申请日:2021-01-08

    IPC分类号: G06F30/15

    CPC分类号: G06F30/15

    摘要: A Rapid Aero Modeling program and process may be applied to computational experiments such as computational fluid dynamics (CFD) programs to obtain aerodynamic models which may be in the form of polynomial equations. The program and process may be utilized to estimate (develop) aerodynamic models appropriate for flight dynamics studies, simulations, and the like. Feedback loops are provided around computational codes to rapidly guide testing toward aerodynamic models that meet user-defined fidelity criteria. A user has the freedom to choose a specific level of fidelity in terms of prediction error, in advance of a CFD test (computation).