Aircraft Stopping Performance Display and Warning
    1.
    发明申请
    Aircraft Stopping Performance Display and Warning 有权
    飞机停止性能显示和警告

    公开(公告)号:US20150120098A1

    公开(公告)日:2015-04-30

    申请号:US14064804

    申请日:2013-10-28

    CPC classification number: G08G5/02 G08G5/0021 G08G5/025

    Abstract: A system and method for determining a predicted stopping performance of an aircraft moving on a runway. A predicted stopping force acting on the aircraft to stop the aircraft is determined by a processor unit as the aircraft is moving on the runway. A predicted deceleration of the aircraft moving on the runway is determined by the processor unit using the predicted stopping force acting on the aircraft to stop the aircraft. The predicted stopping performance of the aircraft on the runway is determined by the processor unit using the predicted deceleration of the aircraft.

    Abstract translation: 一种用于确定在跑道上移动的飞行器的预测停止性能的系统和方法。 当飞机在跑道上移动时,作用在飞机上以阻止飞行器的预测的停止力由处理器单元确定。 在跑道上移动的飞行器的预测减速度由处理器单元使用预测的作用在飞行器上的停止力来确定,以停止飞行器。 飞机在跑道上的预测的停止性能由处理器单元使用飞机预测的减速度来确定。

    Aircraft stopping performance display and warning
    2.
    发明授权
    Aircraft stopping performance display and warning 有权
    飞机停机性能显示和警告

    公开(公告)号:US09082301B2

    公开(公告)日:2015-07-14

    申请号:US14064804

    申请日:2013-10-28

    CPC classification number: G08G5/02 G08G5/0021 G08G5/025

    Abstract: A system and method for determining a predicted stopping performance of an aircraft moving on a runway. A predicted stopping force acting on the aircraft to stop the aircraft is determined by a processor unit as the aircraft is moving on the runway. A predicted deceleration of the aircraft moving on the runway is determined by the processor unit using the predicted stopping force acting on the aircraft to stop the aircraft. The predicted stopping performance of the aircraft on the runway is determined by the processor unit using the predicted deceleration of the aircraft.

    Abstract translation: 一种用于确定在跑道上移动的飞行器的预测停止性能的系统和方法。 当飞机在跑道上移动时,作用在飞机上以阻止飞行器的预测的停止力由处理器单元确定。 在跑道上移动的飞行器的预测减速度由处理器单元使用预测的作用在飞行器上的停止力来确定,以停止飞行器。 飞机在跑道上的预测的停止性能由处理器单元使用飞机预测的减速度来确定。

    Airplane position assurance monitor
    3.
    发明授权
    Airplane position assurance monitor 有权
    飞机位置保证监控

    公开(公告)号:US09257050B2

    公开(公告)日:2016-02-09

    申请号:US14100245

    申请日:2013-12-09

    Abstract: An onboard monitor that ensures the accuracy of data representing the calculated position of an airplane during final approach to a runway. This airplane position assurance monitor is a software function that uses dissimilar sources of airplane position and runway data to ensure the accuracy of the respective data from those dissimilar sources. ILS data and GPS or GPS/Baro data are the dissimilar sources of airplane position data used by this function. This function will calculate the airplane's angular deviations from the runway centerline and from the glide slope with onboard equipment and then compare those angular deviations to the ILS angular deviation information.

    Abstract translation: 一个车载显示器,确保在最后接近跑道时表示飞机计算位置的数据的准确性。 该飞机位置保证监视器是使用不同的飞机位置和跑道数据源的软件功能,以确保来自这些不同来源的各自数据的准确性。 ILS数据和GPS或GPS / Baro数据是该功能使用的飞机位置数据的不同来源。 该功能将计算飞机从跑道中心线和与车载设备的滑行斜率的角度偏差,然后将这些角度偏差与ILS角度偏差信息进行比较。

    Airplane Position Assurance Monitor
    4.
    发明申请
    Airplane Position Assurance Monitor 有权
    飞机位置保证监视器

    公开(公告)号:US20140100720A1

    公开(公告)日:2014-04-10

    申请号:US14100245

    申请日:2013-12-09

    Abstract: An onboard monitor that ensures the accuracy of data representing the calculated position of an airplane during final approach to a runway. This airplane position assurance monitor is a software function that uses dissimilar sources of airplane position and runway data to ensure the accuracy of the respective data from those dissimilar sources. ILS data and GPS or GPS/Baro data are the dissimilar sources of airplane position data used by this function. This function will calculate the airplane's angular deviations from the runway centerline and from the glide slope with onboard equipment and then compare those angular deviations to the ILS angular deviation information.

    Abstract translation: 一个车载显示器,确保在最后接近跑道时表示飞机计算位置的数据的准确性。 该飞机位置保证监视器是使用不同的飞机位置和跑道数据源的软件功能,以确保来自这些不同来源的各自数据的准确性。 ILS数据和GPS或GPS / Baro数据是该功能使用的飞机位置数据的不同来源。 该功能将计算飞机从跑道中心线和与车载设备的滑行斜率的角度偏差,然后将这些角度偏差与ILS角度偏差信息进行比较。

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