Processing method and processor for influence of high-speed aircraft tail flame on data transmission

A high-speed aircraft and data transmission technology, applied in the field of data processing, can solve the problems that the stored data cannot be transmitted wirelessly in real time, the black box cannot be recovered smoothly, and the task cost will be increased, so as to achieve the effects of controlling the development cost, shortening the development time, and reducing the use cost

Active Publication Date: 2020-05-12
BEIJING RES INST OF TELEMETRY +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The advantage of the black box is that it stores a large amount of data. The disadvantage is that the stored data cannot be transmitted wirelessly in real time. It requires separate equipment and strict environmental assessments, which greatly increases the mission cost. Moreover, the black box may not be recovered smoothly due to the impact of the environment and flight trajectory.

Method used

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  • Processing method and processor for influence of high-speed aircraft tail flame on data transmission
  • Processing method and processor for influence of high-speed aircraft tail flame on data transmission
  • Processing method and processor for influence of high-speed aircraft tail flame on data transmission

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Embodiment

[0084] The present invention will be described in detail below with a specific embodiment.

[0085] like image 3 As shown, the control command decomposition module in a high-speed aircraft data delay processor of this embodiment. It includes an inverter A1, a first serial-to-parallel converter A2, a second serial-to-parallel converter A3, and a third serial-to-parallel converter A4.

[0086] The reverse clock signal NBS is connected to the input terminal of the inverter A1. The clock signal BS output from the output terminal of the inverter A1 is connected to the clock terminal of the first serial-to-parallel converter A2, and the control signal N4 is connected to the input terminal of the first serial-to-parallel converter A2. The write command WR is connected to the input terminal of the second serial-to-parallel converter A3, and the input terminal of the first serial-to-parallel converter A2 outputs the clock signal JP4 to be connected to the clock terminal of the secon...

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Abstract

The invention provides a processing method and a processor for influence of high-speed aircraft tail flame on data transmission. The method comprises the following steps: 1) writing real-time data into a memory according to a system rate sequence; 2) reading out the data (delay data) stored in the memory according to a system rate sequence; 3) inserting the delay data into the real-time data through a control signal to form summarized data, and 4) counting the difference between the real-time frame count code and the delay frame count code in the summarized data through a frame count code, andcalculating the delay time of the delay data through a formula.

Description

technical field [0001] The invention relates to a processing method and a processor for data transmission affected by tail flame of a high-speed aircraft, belonging to the technical field of data processing. Background technique [0002] During the flight, the high-speed aircraft needs to send measurement data to the ground receiving equipment in real time. Due to the influence of aircraft engine plume, measurement data cannot be received in real time. Solve the problem of partial data loss and incomplete data caused by intermittent data reception. [0003] At present, the data can be stored in the black box, and it can be completed in the form of finding the black box after the flight mission is completed. The advantage of the black box is that it stores a large amount of data. The disadvantage is that the stored data cannot be transmitted wirelessly in real time. It requires separate equipment and strict environmental assessments, which greatly increases the mission cost...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F3/06G06F12/02G06F13/38G07C5/00
CPCG06F3/0619G06F3/064G06F3/067G06F3/0679G06F12/0246G06F13/385G07C5/008
Inventor 刘祖胜李健杨文涛谢岩肖佳洛刘洪涛
Owner BEIJING RES INST OF TELEMETRY
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