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Real-time Configuration Method of Satellite Communication System Based on Double Buffering Mechanism

A satellite communication system and system configuration technology are applied in the field of real-time configuration of satellite communication systems based on a double buffer mechanism to achieve the effects of reducing user experience, improving flexibility, and reducing the number of restarts

Active Publication Date: 2020-05-26
SPACE STAR TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0008] In view of this, the embodiment of the present invention provides a real-time configuration method of a satellite communication system based on a double buffering mechanism, which solves problems such as improving the flexibility of the current satellite communication system on the premise of maintaining the stability of the satellite communication system

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  • Real-time Configuration Method of Satellite Communication System Based on Double Buffering Mechanism
  • Real-time Configuration Method of Satellite Communication System Based on Double Buffering Mechanism

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Embodiment Construction

[0037] The following description with reference to the accompanying drawings is provided to assist in a comprehensive understanding of various embodiments of the present disclosure as defined by the claims and their equivalents. The following description includes various specific details to aid in understanding, but these are to be regarded as merely exemplary. Accordingly, those of ordinary skill in the art will recognize that various changes and modifications of the various embodiments described herein can be made without departing from the scope and spirit of the disclosure. Also, descriptions of well-known functions and constructions may be omitted for clarity and conciseness.

[0038] The terms and words used in the following description and claims are not limited to the bibliographical meanings, but, are merely used by the inventor to enable a clear and consistent understanding of the present disclosure. Accordingly, it should be apparent to those skilled in the art tha...

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Abstract

The invention discloses a real-time configuration method of a satellite communication system based on double buffering mechanisms. The method comprises the following steps: receiving a real-time configuration instruction, wherein the real-time configuration instruction comprises real-time change configuration; applying the received real-time change configuration to a current system configuration transcript of the satellite communication system; and changing the current system configuration into the real-time change configuration. By adoption of the method, on the premise of ensuring the stability of the satellite communication system, real-time configuration ability of the satellite communication system is provided, thereby greatly improving the flexibly of the system and effectively reducing the restart times of the system and the user experience.

Description

technical field [0001] The invention relates to the technical field of satellite communication, in particular to a real-time configuration method of a satellite communication system based on a double buffer mechanism. Background technique [0002] Compared with the Internet and mobile networks, satellite communication has irreplaceable characteristics. Satellite communication does not require special wiring, nor does it need to build base stations in various places. Instead, it only needs to build a central earth station and set up terminal stations in places to communicate. End stations are now portable and end stations can be easily relocated. Satellite communication has a large coverage area, and it is very marketable in some areas where it is not convenient to build base stations or wiring, such as sea and remote mountainous areas. [0003] Satellite communication systems are generally divided into main stations, satellites and terminal stations. The main station is con...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H04B7/185
CPCH04B7/1851H04B7/18519H04B7/18573
Inventor 李海林杨锴姬晓慧刘竞超曹田熠尤启迪杨博张华健石云
Owner SPACE STAR TECH CO LTD
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