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发明公开
CN109353531A 飞机降落导航系统 审中-实审

飞机降落导航系统
摘要：
本发明涉及一种无线电技术，具体涉及飞机降落导航系统。飞机降落导航系统，包括设置于飞机上的陀螺仪、无线电高度表、信号传输模块、激光发射装置、设置于降落跑道的接收面板、信号处理塔，所述陀螺仪、无线电高度表通过信号传输模块与信号处理塔信号连接，接收面板接收激光发射装置发射的激光后与信号处理塔信号连接。本发明能够及时根据飞机降落的姿态做出即时调整，从而提高飞机降落的安全性。
摘要（英）：

The invention relates to radio engineering, in particular to an aircraft landing navigation system. The aircraft landing navigation system comprises a gyroscope, a radio altimeter, a signal transmission module, a laser emission device, a receiving panel and a signal processing tower, wherein the gyroscope, the radio altimeter, the signal transmission module and the laser emission device are arranged on an aircraft; the receiving panel and the signal processing tower are arranged on a landing runway; the gyroscope and the radio altimeter are in signal connection with the signal processing towerthrough the signal transmission module, and the receiving panel receives laser emitted by the laser emission device and then is in signal connection with the signal processing tower. By means of theaircraft landing navigation system, instant adjustment can be made in real time according to the aircraft landing attitude, and therefore, the aircraft landing safety is improved.

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