Ground data transmission antenna layout method adapting to inter-satellite transmission

A technology for ground-to-ground data transmission antennas and data transmission antennas, which is suitable for antennas, antennas, and antenna parts on movable objects, and can solve the problem that data transmission antennas are not suitable for multi-satellite flying around the left and right side-to-side inter-satellite data Transmission and other issues, to achieve the effect of effective transmission, high applicability, and enhanced inter-satellite transmission airspace

Active Publication Date: 2020-10-16
SHANGHAI SATELLITE ENG INST
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Problems solved by technology

[0005] As in-orbit applications such as high and low orbit satellites and constellation networking continue to be proposed in the field of communication, the existing data transmission antenna single-to-grou...

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  • Ground data transmission antenna layout method adapting to inter-satellite transmission
  • Ground data transmission antenna layout method adapting to inter-satellite transmission
  • Ground data transmission antenna layout method adapting to inter-satellite transmission

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Embodiment Construction

[0040] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several changes and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0041] In order to solve the configuration and layout engineering problems of space vehicles such as multi-satellite ground-to-ground data transmission antenna half-airspace communication link building, star multi-component interference occlusion, and extending parts beyond the space of the launch vehicle fairing, according to the characteristics of ground-to-ground data transmission antenna, an adaptive Research on the new configuration layout design optimization method for inter-satellite data transmis...

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Abstract

The invention provides a ground data transmission antenna layout method adapting to inter-satellite transmission. The method comprises the following steps: firstly, determining the requirements of a data transmission antenna on an on-orbit operation satellite for ground and inter-satellite data transmission, secondly, determining the installation position and the axis direction of the data transmission antenna on the on-orbit operation satellite, and finally, determining the connection mode of the data transmission antenna and the on-orbit operation satellite to ensure that the data transmission antenna is not shielded. According to the method provided by the invention, the problems that in the process of multiple satellites fly along and fly around in constellation networking, beam shielding of an on-orbit semi-airspace inter-satellite data transmission antenna of a satellite, interference between the data transmission antenna and a ground load and a solar array, and the narrow configuration layout of a space in a fairing during launching are solved. The beneficial effects of half-airspace data transmission, multi-component interference elimination and adaptation to the internalspace of the fairing are achieved, a selection mode with high expansion capacity and high applicability is provided, and high universality is achieved.

Description

technical field [0001] The present invention relates to space vehicle configuration and layout design, ground and on-orbit communication signal data transmission, and multi-constraint system integration and compatibility technologies. Specifically, it relates to a ground-to-ground data transmission antenna layout method suitable for inter-satellite transmission, especially to A layout method for ground-to-ground data transmission antennas on a satellite that satisfies the internal accommodation space of the launch vehicle fairing and meets the requirements of inter-satellite data transmission. Background technique [0002] In the future, spacecraft will develop in the direction of large-scale, multi-functional, performance expansion and high integration. The salient features of these spacecraft in the process of configuration and layout mainly include: larger size envelope requirements, wider detection range, more prominent interference and occlusion problems, and layout opt...

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Application Information

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IPC IPC(8): H01Q1/28
CPCH01Q1/288
Inventor 顾永坤冯彦军曹岸杰黄业平仲惟超张国强
Owner SHANGHAI SATELLITE ENG INST
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