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On-orbit Calibration System and Method for High Gain Antenna in Deep Space Exploration

A high-gain antenna and deep-space detection technology, applied in the field of on-orbit calibration systems, can solve problems such as the impact of ground pointing accuracy errors, affecting pointing accuracy, high-gain antenna pointing accuracy errors, etc., to achieve the elimination of ground pointing errors, The effect of increasing the gain value

Active Publication Date: 2021-04-13
SHANGHAI SATELLITE ENG INST
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

High-gain antennas are usually large-diameter parabolic antennas. On-orbit sunlight and on-orbit maneuvering will cause stress, which will cause micro-deformation of high-gain antennas and affect the ground pointing accuracy
[0003] Due to the high gain of the high-gain antenna and the narrow beam width pointing to the ground, the pointing accuracy error of the high-gain antenna and the excessive error of the pointing accuracy of the entire detector system may seriously affect the antenna-to-ground communication

Method used

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  • On-orbit Calibration System and Method for High Gain Antenna in Deep Space Exploration
  • On-orbit Calibration System and Method for High Gain Antenna in Deep Space Exploration
  • On-orbit Calibration System and Method for High Gain Antenna in Deep Space Exploration

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Embodiment Construction

[0022] 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 modifications and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0023] like figure 1 As shown, the on-orbit calibration system of the high-gain antenna for deep space detection of the present invention adopts the ground station and the receiving detector of the ground station. The carrier radio frequency signal is used to find out the moment when the signal is the strongest, and the ground station receives the detector to invert to give the position pointing to the space at this moment. The high-gain antenna of the ground station receiving detector points to ...

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Abstract

The invention provides an on-orbit calibration system and method for a high-gain antenna for deep space detection. The high-gain antenna for deep space detection on-orbit calibration system uses a ground station and a ground station receiving detector. The ground station mainly provides high-sensitivity Receiver and large antenna, the ground station receiving detector transmits a single beacon or residual carrier radio frequency signal, finds out the moment when the signal is the strongest, and inverts the pointing space position at this moment through the ground station receiving detector. The invention carries out the on-orbit calibration of the antenna, eliminates the pointing error of the high-gain antenna to the ground during the long-term flight of the detector on the orbit, and improves the gain value of the communication link.

Description

technical field [0001] The invention relates to an on-orbit calibration system and method, in particular to an on-orbit calibration system and method for high-gain antennas for deep space exploration, which can be applied to deep space explorations such as Mars, Venus, and Saturn. Background technique [0002] Deep space exploration relies on high-gain antennas to improve ground-to-ground communication capabilities. During the period when the antenna is in orbit, it needs to receive ground uplink commands, and at the same time send detector-related data to the ground. High-gain antennas are usually large-diameter parabolic antennas. On-orbit sunlight and on-orbit maneuvering will cause stress, which will cause micro-deformation of high-gain antennas and affect the ground pointing accuracy. [0003] Due to the high gain of the high-gain antenna and the narrow beam width pointing to the ground, the pointing accuracy error of the high-gain antenna and the excessive error of th...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H04B7/185H04B17/20H04J3/06
CPCH04B7/1851H04B7/18517H04J3/0638H04B17/20
Inventor 李金岳牛俊坡王伟陆希褚英志
Owner SHANGHAI SATELLITE ENG INST
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