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A multi-routing inter-satellite communication link based on cluster formation

A technology of communication link and routing star, which is applied in the field of aerospace vehicles, can solve the problems of not yet collecting data, not finding instructions or reports, etc., to ensure timeliness and continuity, reduce forwarding delay, and avoid interruption of information exchange Effect

Active Publication Date: 2020-11-13
SHANGHAI SATELLITE ENG INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0004] At present, there is no description or report of the similar technology of the present invention, and no similar data at home and abroad have been collected yet.

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  • A multi-routing inter-satellite communication link based on cluster formation
  • A multi-routing inter-satellite communication link based on cluster formation

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Embodiment Construction

[0017] In order to make the objects and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the examples. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0018] Such as figure 1 As shown in , the embodiment of the present invention provides a multi-routing inter-satellite communication link based on cluster formation, and the multi-routing inter-satellite communication link suitable for cluster formation is dedicated to omnidirectional It is composed of a communication antenna for signal transmission and reception, an inter-satellite terminal dedicated to multi-channel search / acquisition / tracking, and a processor dedicated to inter-satellite data transmission and reception, screening and other preprocessing tasks; the multi-routing inter-satellite communication link adopts multi-channel Parallel...

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Abstract

The invention discloses a multi-route inter-satellite communication link based on cluster formation. The multi-route inter-satellite communication link based on the cluster formation is composed of acommunication antenna which is exclusively used for omnidirectional signal transmitting and receiving; inter-satellite terminal machines which are exclusively used for multichannel searching / capturing / capturing; and processor which are exclusively used for inter-satellite data transmitting and receiving and screening. According to the multi-route inter-satellite communication link, through adoption of a multichannel parallel capturing technology, the same cluster satellite signal is searched; through utilization of a queue type multi-route communication technology, inter-satellite informationof all satellites in a cluster is directly or indirectly switched; through adoption of a forwarding delay dynamic optimization technology, the processors determine transmitting opportunity according to priority of current data and reduce forwarding delay of important data to the lowest; and a multiway information optimization technology is employed. According to the multi-route inter-satellite communication link, the problem that a traditional inter-satellite communication scheme is few in access terminal number, serious in dependence on antenna visibility and long in forwarding delay is solved.

Description

technical field [0001] The invention relates to an aerospace vehicle, in particular to a cluster formation-based multi-routing inter-satellite communication link. Background technique [0002] In order to meet the needs of inter-satellite multi-route communication for multi-satellite cluster formations, the design of inter-satellite communication link multi-route communication technology is carried out for the requirements of queue communication and multi-satellite communication. [0003] There are many inter-satellite communication link design schemes available for reference at home and abroad, but these inter-satellite links are suitable for inter-satellite communication with a small number of satellites or multi-satellite inter-satellite links with constant direction, or only for visible stars in the field of view. Communication, or the forwarding delay between multiple stars is relatively large, or the inter-satellite link gap between multiple stars does not meet the cur...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H04B7/185
CPCH04B7/18521
Inventor 陈重华李楠温俊健叶兴彬刘艳阳高俊英赵彦
Owner SHANGHAI SATELLITE ENG INST
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