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C-band network transceiving system based on time division duplex

A network transceiver, time division duplex technology, applied in the field of communication, can solve the problems of poor real-time performance, incompatibility, and less information transmission.

Active Publication Date: 2020-05-29
CHENGDU KSW TECH
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] For a long time, in the test flight stage of the test aircraft, the real-time data monitoring method is single, the transmission of information is less, and the real-time performance is poor. There are many inconveniences in timely handling of aircraft failures in the air, flight quality monitoring, and auxiliary flight command. extremely uncomfortable

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  • C-band network transceiving system based on time division duplex
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Embodiment Construction

[0143] The technical solution of the present invention will be further described in detail below in conjunction with the accompanying drawings, but the protection scope of the present invention is not limited to the following description.

[0144] A C-band network transceiver system based on time-division duplexing is a key device used for flight test data transmission of the test machine when the test machine is flying.

[0145] In terms of application requirements for flight test data transmission, using the existing basic technology of C-band broadband wireless network link, combined with the design idea of ​​cellular mobile communication, the design scheme of C-band network transceiver equipment is proposed, and the overall structure and functions of the system are determined. The development idea of ​​the subsystem has formed the directional guidance document for equipment development, and determined the architecture design of the C-band network transceiver system using th...

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Abstract

The invention discloses a C-band network transceiving system based on time division duplex, and relates to the technical field of communication. The system comprises an airborne end telemetering and remote control unit, wherein the airborne end telemetering and remote control unit comprises an airborne end C-band broadband network transceiver and an airborne end C-band power amplifier, and has thefunctions of network access, network quitting, parameter setting and state detection; and a ground base station type telemetry and telecontrol unit which is composed of a ground end C-band broadbandnetwork transceiver and a base station type C-band power amplifier, and has data transmission functions of TDD duplex data transmission, state detection and parameter setting. The design scheme of theairborne telemetry and telecontrol unit and the ground base station type telemetry and telecontrol unit solves the problem of air-ground real-time high-speed data transmission. Flight inspection shows that the cross-linking relation between the system and the original aircraft equipment is correct, the normal work of the original aircraft equipment is not influenced, the system function is normal, the performance index meets the design requirement, and a solid foundation is laid for the deepening application of subsequent flight data.

Description

technical field [0001] The invention relates to the technical field of communication, in particular to a time-division duplex-based C-band network transceiver system. Background technique [0002] For a long time, in the test flight stage of the test aircraft, the real-time data monitoring method is single, the transmission of information is less, and the real-time performance is poor. There are many inconveniences in timely handling of aircraft failures in the air, flight quality monitoring, and auxiliary flight command. Very uncomfortable. Therefore, by collecting the flight data of the aircraft flight test parameters in real time and downloading them to the ground, the real-time transmission of the aircraft flight data will be realized, which will further expand the application range of the flight data, and then achieve real-time monitoring of important parameter indicators of the test aircraft, and actively respond to emergencies. It is of great significance to ensure t...

Claims

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Application Information

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IPC IPC(8): H04J3/06H04L12/24H04B7/185H04Q9/04
CPCH04B7/18506H04B7/18517H04J3/0667H04L41/0213H04L41/046H04Q9/04
Inventor 张吉林冯川王维陈开国陈世朴王敏石璞
Owner CHENGDU KSW TECH
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