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Apparatus for an automated aerial refueling boom using multiple types of sensors

机译:使用多种传感器的自动空中加油机的装置

摘要

A system for automated control of a refueling boom coupled to a tanker aircraft is provided. The system includes: a first inertial measurement unit (IMU) providing inertial measurements for the tanker aircraft; a first GPS receiver providing a GPS location for a GPS antenna attached to the tanker aircraft; and a processor adapted to calculate a first inertial navigation state for the tanker aircraft through integration of the inertial measurements, the processor being further adapted to calculate a first inertial navigation state error relative to the GPS location and to filter the first inertial navigation state error and the first inertial navigation state based upon noise characteristics of the first IMU and the first GPS receiver to provide an updated inertial navigation state for the tanker aircraft, the processor being further adapted to control the refueling boom relative to a receiver aircraft based upon the first and updated inertial navigation states.
机译:提供了一种用于自动控制联接到加油机的加油机的系统。该系统包括:第一惯性测量单元(IMU),其为加油机提供惯性测量;以及第一GPS接收器,其提供用于附接到加油机的GPS天线的GPS位置;以及适于通过对惯性测量值进行积分来计算油轮飞机的第一惯性导航状态的处理器,该处理器还适于计算相对于GPS位置的第一惯性导航状态误差并过滤第一惯性导航状态误差和所述第一惯性导航状态基于所述第一IMU和所述第一GPS接收器的噪声特性以为所述加油机提供更新的惯性导航状态,所述处理器还适于基于所述第一和第二控制相对于接收器飞机控制加油臂。更新了惯性导航状态。

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