Integrated navigation system tester

A combined navigation system and tester technology, applied in the field of aircraft testing, can solve problems such as insufficient precision, poor reliability, and large differences, and achieve the effects of good reliability, reasonable design, and large differences

Inactive Publication Date: 2017-01-04
HARBIN
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0002] The existing integrated navigation system test equipment is mainly applicable to the working mechanism of the traditional gyroscope, which has great differences, insufficient precision, poor reliability, often inaccurate test data, no on-board simulation state, and can not meet the relevant test requirements

Method used

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specific Embodiment approach

[0009] Specific embodiments: the present invention will be further described in detail below in conjunction with the appendix.

[0010] The tester of the present invention includes a power controller (1), a data acquisition switch unit (2), a detection adapter (3), an automatic tester (4), a main control machine simulator (5) and a test cabinet (6); wherein, The finished product of integrated navigation is connected to the test cabinet (6) through the detection adapter (3), the main control machine simulator (5) loads the analog signals required for the test to the test cabinet (6), and the power controller (1) provides the entire test system Power supply, data acquisition switch unit (2), and automatic tester (4) are connected with the integrated navigation system through adapter conversion, and the data is sent to the test cabinet after communication processing, and the control signal can be input to the external product to be tested, and the test personnel can simultaneously...

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Abstract

The invention discloses an integrated navigation system tester. The integrated navigation system tester comprises a power controller (1), a data collection switch unit (2), a detection adaptor (3), an automatic tester (4), a main control computer simulator (5) and a test equipment cabinet (6), wherein an integrated navigation finished product is connected to the test equipment cabinet (6) through the detection adaptor (3), the main control computer simulator (5) loads all analog signals needed by testing to the test equipment cabinet (6), the power controller (1) provides power for the whole testing system, the data collection switch unit (2) and the automatic tester (4) are connected with the integrated navigation system through conversion of the adaptor, data are sent to the testing equipment cabinet through communication processing, control signals can be input into an external finished product to be tested, and testing staff can carry out input set on the testing through the testing equipment cabinet. The integrated navigation system tester is reasonable in design, the integrated navigation system installed in a certain type of machine in a factory adopts laser inertial navigation, and a laser gyro has great work mechanism difference from a traditional gyro and is higher in accuracy and reliability. The test method research is product performance testing based on test room conditions, and the check before product installation is achieved.

Description

technical field [0001] The invention belongs to the technical field of aircraft testing, and relates to an integrated navigation system tester. Background technique [0002] The existing integrated navigation system test equipment is mainly applicable to the working mechanism of the traditional gyroscope, which has great differences, insufficient precision, poor reliability, often inaccurate test data, no on-board simulation state, and can not meet the relevant test requirements. The integrated navigation system tester of the present invention has higher simulation signal accuracy, can simultaneously simulate the cross-linking of the on-board system and the finished product of the combined navigation, can complete all performance and function tests of the combined navigation system, and fully meets the laboratory test requirements of the finished product. Contents of the invention [0003] Purpose of the present invention: The integrated navigation system installed in a ce...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01C25/00
CPCG01C25/00
Inventor 王海涛朱希谭飞邵丽红
Owner HARBIN
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