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公开(公告)号:US09279683B2
公开(公告)日:2016-03-08
申请号:US14382182
申请日:2013-03-02
Applicant: Moog Inc.
Inventor: Martin A. Turon , Darren S. Liccardo
CPC classification number: G01C19/56 , B64D43/00 , H04Q9/00 , H04Q2209/00
Abstract: A low power method for determining whether a cargo destined for air transport is in a flying state having the steps of: providing a housing for attachment to a cargo the housing having: an accelerometer for detecting a linear acceleration, a gyroscope for detecting an angular rate, a controller measuring a linear acceleration with the accelerometer, measuring an angular rate with the gyroscope, providing the measured linear acceleration and angular rate to the controller, and generating a flight status output signal indicating whether the housing is in a flying state as a function of the linear acceleration signal and angular rate signal.
Abstract translation: 用于确定用于航空运输的货物是否处于飞行状态的低功率方法具有以下步骤:提供用于附接到货物的壳体,该壳体具有:用于检测线性加速度的加速度计,用于检测角速率的陀螺仪 ,用加速度计测量线性加速度的控制器,用陀螺仪测量角速率,向所述控制器提供所测量的线性加速度和角速度,以及产生指示所述壳体是否处于飞行状态的飞行状态输出信号 的线性加速度信号和角速度信号。
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公开(公告)号:US20150027226A1
公开(公告)日:2015-01-29
申请号:US14382182
申请日:2013-03-02
Applicant: Moog Inc.
Inventor: Martin A. Turon , Darren S. Liccardo
CPC classification number: G01C19/56 , B64D43/00 , H04Q9/00 , H04Q2209/00
Abstract: A low power method for determining whether a cargo destined for air transport is in a flying state having the steps of: providing a housing for attachment to a cargo the housing having: an accelerometer for detecting a linear acceleration, a gyroscope for detecting an angular rate, a controller measuring a linear acceleration with the accelerometer, measuring an angular rate with the gyroscope, providing the measured linear acceleration and angular rate to the controller, and generating a flight status output signal indicating whether the housing is in a flying state as a function of the linear acceleration signal and angular rate signal.
Abstract translation: 用于确定用于航空运输的货物是否处于飞行状态的低功率方法具有以下步骤:提供用于附接到货物的壳体,该壳体具有:用于检测线性加速度的加速度计,用于检测角速率的陀螺仪 ,用加速度计测量线性加速度的控制器,用陀螺仪测量角速率,向所述控制器提供所测量的线性加速度和角速度,以及产生指示所述壳体是否处于飞行状态的飞行状态输出信号 的线性加速度信号和角速度信号。
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