Radio compass system test adapter

Abstract

The invention relates to radio compass system test, in particular to a radio compass system test adapter. The radio compass system test adapter comprises a first connector and a second connector, the first connector is provided with at least five pins, the five pins of the first connector are respectively connected with five channels of input signals of a receiver, the second connector is provided with at least 41 pinholes, and the pinhole K of the second connector is connected with a pin K of a radio magnetic indicator; the pinhole M of the second connector is connected with a pin M of a radio magnetic indicator; the pinhole N of the second connector is connected with a pin N of a radio magnetic indicator; the pinhole P of the second connector is connected with a pin P of a radio magnetic indicator; the pinhole L of the second connector is connected with a pin L of a radio magnetic indicator; the pinhole S of the second connector is connected with a pin S of a radio magnetic indicator; the pinhole V of the second connector is connected with a pin V of a radio magnetic indicator; the pinhole T of the second connector is connected with a pin T of a radio magnetic indicator.

Description

technical field [0001] The invention relates to a radio compass system test, in particular to a radio compass system test adapter. Background technique [0002] When testing the radio compass system before installation, it is necessary to test the performance indicators of its orientation function parameters. The usual method is to connect the wireless electromagnetic indicator of different systems or the instrument equivalent to the aircraft azimuth indication to the radio compass system, and the detection system The azimuth indication data (X, Y, Z) is output synchronously. This method is complicated to operate, and the limitations of the supporting test of the finished product are strong, which is not conducive to the rapid and effective fault location and troubleshooting when the airborne parts fail. Contents of the invention [0003] The purpose of the present invention: to provide a radio compass system test adapter, which can make different types of wireless electro...

AI Technical Summary

Problems solved by technology

[0002] When testing the radio compass system before installation, it is necessary to test the performance indicators of its orientation function parameters. The usual method is to connect the wireless electromagnetic indicator of different systems or the instrument equivalent to the aircraft azimuth indication to the radio compass system, and the detection system The azimuth indication data (X, Y, Z) are output synchronously. This method is complicated to operate, and the limitations of the supporting test of the finished product are strong, which is not conducive to fast and effective fault location and troubleshooting when the airborne parts fail.

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