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DCS system satellite link downlink data confirmation frame transmission method

A satellite data and downlink data technology, applied in the field of satellite communication, can solve the problem of limiting the number of ground DCPs

Active Publication Date: 2017-05-10
BEIJING UNIV OF POSTS & TELECOMM
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] The traditional confirmation method is to confirm the ground DCP data sequentially. As the number of DCPs increases, the confirmation time also increases linearly. The overhead time of DCS satellites is about 20 minutes, which limits the number of ground DCPs.

Method used

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  • DCS system satellite link downlink data confirmation frame transmission method
  • DCS system satellite link downlink data confirmation frame transmission method

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Experimental program
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Embodiment Construction

[0016] A. Downlink data confirmation frame format design

[0017] The present invention designs a variable-length downlink confirmation frame format, designs the meaning of the service flag, and designs the length of the variable-length ID flag and the meaning of the data information word.

[0018] The present invention proposes a variable-length frame structure. A dcs system has m dcps, and the satellite ID marking needs Bit. Such as figure 1 The structure of the downlink confirmation frame is shown, including 2-bit service indicator, 2-bit variable-length coding method indicator, 0~ Bit variable length satellite ID mark and 4-bit data information word. Assuming that m is 60,000, the variable-length satellite ID flag is 16 bits.

[0019] The service flag bit is used to indicate unicast, broadcast, and multicast modes. For example, the highest two digits are 11, indicating that the following address is a multicast address; if it is 00, the following address is a unicast address; i...

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Abstract

The invention discloses a satellite link downlink data acknowledgement frame format and transmission method in a satellite DCS. The method includes the steps that A, the acknowledgement frame format is a variable-length frame format of a down link transmission acknowledgement data frame of a DCS satellite system, and the frame format is composed of a service identification, a bit variable-length satellite ID bit and a data information word identification; B, the acknowledgement frame transmission method is a down link acknowledgement frame transmission method based on the combination of a multicast and unicast hybrid transmission mode and a variable-length acknowledgement frame format compression technique. When the physical distance of a DCP is short, the DCP can be joined into the same multicast group, a multicast mode is used for conducting group confirmation, otherwise a unicast mode is adopted, compressed optimization is carried out on the down link acknowledgement frame, and optimized compression is achieved by the way that bit compression, amplitude coding and variable-length compressed encoding are combined. The variable-length frame format is flexible in design, and the transmission method is easy to implement and efficient.

Description

[0001] 1 technical field [0002] The invention is designed in the field of satellite communications, and relates to a multi-terminal satellite data acquisition system (DCS) satellite data acquisition system. [0003] 2 background technology [0004] The data acquisition system (DCS) in satellite communications is a system that collects data or locates the data acquisition platform through a remote data acquisition platform. It uses aerospace technologies such as telemetry, remote control and remote monitoring, and transmits the various monitoring data collected by the remote data acquisition platform to the ground receiving processing center through satellite real-time or storage and forwarding, and finally the data processing center delivers the data to User use. Although hundreds or even thousands of data collection platforms are geographically dispersed, they are organically linked through the DCS system and work together to complete a monitoring task. Most of the data collecti...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H04L1/00H04B7/185
Inventor 张琦忻向军田清华刘博王拥军张丽佳李逍樊俊南陈天双杨澍李伟斌齐小航
Owner BEIJING UNIV OF POSTS & TELECOMM