Systems and methods for providing throttle guidance as a function of flight path acceleration

    公开(公告)号:US11299285B2

    公开(公告)日:2022-04-12

    申请号:US16672105

    申请日:2019-11-01

    Abstract: Technologically improved vehicle control systems and methods are described. The provided vehicle control systems and methods embody an inner loop auto-throttle control for causing delta-throttle changes, i.e., servo changes, to achieve desired acceleration targets. The system generates an error on a potential flight path angle using a received thrust acceleration command. The error on the potential flight path angle is converted into an equivalent acceleration. A throttle rate command TLA_ratecmd is generated by converting the equivalent acceleration into the throttle rate command TLA_ratecmd.

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