Experimental comprehensive control and management system and method

A comprehensive control and management system technology, applied in the field of engineering testing, can solve the problems of long test period, low test efficiency, lack of data transmission and sharing means, etc., and achieve a reasonable and compact structure, good scalability, and shorten the large-scale test cycle. Effect

Active Publication Date: 2018-02-23
XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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  • Application Information

AI Technical Summary

Problems solved by technology

However, in the test of aircraft functional systems, it usually requires multiple devices to be used at the same time and work in a coordinated manner, which can only be completed by the coordination of operators. In addition, there is a lack of effective and consistent means of data transmission and sharing between devices , leading to low test efficiency and long test cycle

Method used

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  • Experimental comprehensive control and management system and method
  • Experimental comprehensive control and management system and method
  • Experimental comprehensive control and management system and method

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Embodiment Construction

[0032] In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below in conjunction with the drawings in the embodiments of the present invention. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the invention. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention. Embodiments of the present invention will be described in detail below ...

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Abstract

The invention discloses an experimental comprehensive control and management system, and belongs to the technical field of engineering experiments. The system is composed of an operation control layer, a video / audio monitoring and scheduling layer, a data exchange transmission layer, a device operating layer and a power distribution control and management layer. Remote control, state setting and data information exchange are conducted by the operation control layer on devices in the device operating layer through the data exchange transmission layer, and the data information of the devices inthe device operating layer is stored; the operation control layer is connected with the video / audio monitoring and scheduling layer so as to conduct transmission and information sharing on the data information of the devices in the device operating layer and an airplane function system undergoing experiments through audio signals and video signals; the operation control layer is connected with thepower distribution control and management layer, and power is supplied to the devices and the power supply operation states of the devices are monitored through the power distribution control and management system. The intelligent, networked, informational and digitized experimental comprehensive control and management technical scheme is adopted, the experimental efficiency is improved, and theexperimental period is shortened.

Description

technical field [0001] The invention belongs to the field of engineering test technology, and in particular relates to a test comprehensive control management system and method. Background technique [0002] In the design and development of aircraft, especially in the design and development of important functional systems of aircraft, it is often necessary to carry out various tests, such as: flight control system iron bird integration test, hydraulic system integration iron bird test, landing gear system iron bird Integration test, integration test of avionics system, etc. In the above tests, in order to complete a comprehensive and systematic inspection and test of the aircraft functional system, it is usually necessary to develop a corresponding test environment based on the test object - the aircraft functional system - such as the flight control system, and according to the test inspection and test items Content, to carry out related tests such as the coordination and ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/60G06F17/50
CPCB64F5/60G06F30/20
Inventor 支超有李美玲李经纬
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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