Testing System for Attitude Heading Reference System of Aircraft

摘要

The present invention relates to an attitude reference device bearing the test system of the aircraft, more specifically, of the aircraft A system for testing the position bearing the reference device, fixing the position bearing the reference apparatus, the three-dimensional position based on the orientation device is receiving a driving signal applied to the roll of a particular state in accordance with the driving signal, so as to have a pitch and heading and the state apparatus to perform the simulation with animated features; Condition simulation device and is connected to the position bearing the reference device fixed to the condition simulation device, a specific tester from roll, pitch and heading, and applied to the state of the test conditions, after receiving the data, and generates a driving signal condition simulation device, position orientation that receives an output value sent from the reference devices is detected by the position bearing the reference roll, to a position of the aircraft azimuth reference device test system consisting of a control device for displaying the displacement pitch and heading. ; According to the present invention, by using a fixing device in which the back control state simulation unit directly mounted to the aircraft without the aircraft attitude reference device bearing the test bench can be simply moved. ; Accordingly, the prior many people have to take part in the examination of the position bearing the reference device, such as can not eliminate the consumption of unnecessary manpower, not only shortening the test time, has the advantage of improving the reliability of the test Fig.