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A black box and monitoring method for multi-node state monitoring data carried by aircraft

A technology for monitoring data and aircraft, applied in the direction of data exchange through path configuration, data exchange network, instruments, etc., can solve problems such as high noise tolerance, data loss, and loss of lock at LOCK, so as to reduce recovery time and improve Reliability, the effect of solving the problem of loss of lock

Active Publication Date: 2022-02-11
ZHONGBEI UNIV
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Problems solved by technology

The LVDS serial bus has very low voltage swing, high noise tolerance, power consumption is only a few milliwatts, and the transmission rate can reach hundreds of Mbps. Compared with other buses, it has certain advantages, but in the LVDS serial bus During the bus communication process, the receiving end repeatedly receives 4 identical data continuously, and there will be a loss of lock at the LOCK, resulting in data loss

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  • A black box and monitoring method for multi-node state monitoring data carried by aircraft
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  • A black box and monitoring method for multi-node state monitoring data carried by aircraft

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Embodiment Construction

[0027] The present invention will be further described in conjunction with the accompanying drawings and embodiments.

[0028] Depend on figure 1As shown, the aircraft carrying multi-node state monitoring data black box provided by the present invention is used for dynamic testing and recording the parameters of various parts of the aircraft, including more than two data acquisition devices, LVDS serial bus, CAN bus, cable terminal resistance and setting It consists of a storage server that manages the dispatch center. Each editor i is equipped with two buffers i-1 and i-2, i is the number of the editor, 1≤i≤n, forming a double buffer structure, the editor is used to collect the measured signals of each cabin or position of the aircraft, And the collected and encoded data is stored in the buffer. The editor has two types of interfaces, one is the electrical interface with the specific test object, and the other is the electrical interface with the LVDS serial bus and the CAN ...

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Abstract

The invention provides a multi-node state monitoring data black box and monitoring method carried by an aircraft, which are used for dynamic monitoring and recording of parameters of various parts of the aircraft. The data black box includes more than two data acquisition and editing devices, LVDS serial bus, and CAN bus , cable terminal resistance and a storage server with a management dispatch center; each editor has two types of interfaces and is equipped with two buffers, and the buffer of the editor is connected to the management dispatch center of the storage server through the LVDS serial bus , the LVDS serial bus is used to transmit data, and the CAN bus is used to transmit status command information; through repeated monitoring of data, the problem of LVDS bus out-of-lock is solved to avoid data loss; Synchronize the clocks, and then achieve the purpose of unifying the clocks of the editors, efficient use of cabin space and reduction of black box recovery time.

Description

technical field [0001] The invention relates to a multi-node state monitoring data black box carried by an aircraft and a monitoring method, belonging to the field of aerospace testing. Background technique [0002] The test system is an indispensable part of the space vehicle test, and the data black box is the only test method for the space vehicle to test the system when it is in the launch tube, underwater or returning to the "black barrier area" of the atmosphere. With the continuous development of aerospace test technology, the types and quantities of data black boxes in the test system are gradually increasing. However, the data black boxes placed in each compartment or position do not have any electrical and communication connection with each other, resulting in the clocks of each data black box not being able to be accurately unified. There are many instruments in the black box of on-site test data, which reduces the reliability of the test and increases the cost, ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G07C5/08H04L12/40
CPCG07C5/08H04L12/40006H04L2012/4028H04L2012/40215
Inventor 张彦军刘召军
Owner ZHONGBEI UNIV
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