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Non-measurement-and-control arc segment shadow period thermal control compensation power saving method and system

A technology for compensating power and arc segments, applied in the field of satellites, can solve the problems of increasing the burden, increasing the risk of battery over-discharge, and the failure of satellite commands to uplink, etc., to reduce the risk of over-discharge, save thermal control compensation power, and ensure the entire satellite Effect of temperature level

Active Publication Date: 2020-05-01
SHANGHAI SATELLITE ENG INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

During the shadow period, the satellite has no light, and the thermal control compensation power increases, which forms an irreconcilable contradiction with the decrease of battery capacity
In addition, in the non-measurement and control arc section, the satellite command cannot go up, and the thermal compensation heater cannot be effectively controlled. The increased burden on the battery during the shadow period also increases the risk of battery over-discharge.

Method used

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  • Non-measurement-and-control arc segment shadow period thermal control compensation power saving method and system

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Embodiment Construction

[0033] 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.

[0034] The present invention provides a thermal control compensation power saving method in the shadow period of the satellite non-measurement and control arc segment. The specific implementation process can be found in figure 1 , where T1 is the start time of the non-measurement and control arc, and the time before T1 is the measurement and control arc; T2 is the time of satellite image entry of the non-measurement and control arc; T3 is the time of satellite image emission of the non-measurement and co...

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PUM

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Abstract

The invention provides a non-measurement-and-control arc segment shadow period thermal control compensation power saving method. The method comprises the steps of 1, determining a satellite illumination period heater state and a shadow period heater state through thermal simulation, 2, in the satellite measurement and control arc section, sending a thermal control heater program control forbiddinginstruction and a thermal control heater state setting instruction according to the illumination period heater state, 3, sending a delay instruction with a time code according to the shadow time forecast and the shadow period heater state of the non-measurement-and-control arc section before the satellite goes out of the measurement-and-control arc section and enters the non-measurement-and-control arc section, and respectively setting the thermal control heater states of the non-measurement-and-control arc section when the non-measurement-and-control arc section goes into the shadow and goesout of the shadow, and 4, after the non-measurement-and-control arc section is finished and the satellite enters the measurement-and-control arc section again, sending a program control permission instruction of the thermal control heater, and carrying out closed-loop control on the heater according to a threshold value. Thus, the thermal control compensation power of the satellite in the shadowperiod is effectively saved, and the over-discharge risk of the storage battery is greatly reduced.

Description

technical field [0001] The present invention relates to the field of satellite technology, in particular to a method and system for saving power by thermal control compensation during the shadow period of a non-measurement and control arc segment. In particular, it relates to a power saving method for thermal control compensation during the shadow period of a satellite non-measurement and control arc. Background technique [0002] During the light period of the satellite in orbit, the solar battery array equipped with the star can provide energy for the whole star; while in the shadow period, the battery needs to meet the power consumption demand of the whole star. However, with the development of spaceflight, it is urgent to optimize resources such as the weight and power consumption of satellites. The weight of batteries is also strictly controlled, and their power generation is also reduced accordingly. During the shadow period, the satellite has no light, and the therma...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/10B64G1/50B64G1/22
CPCB64G1/10B64G1/22B64G1/50
Inventor 顾燕萍赵吉喆杨牧孙伟伟黄小虎高勇蒋孟虎陈修桥
Owner SHANGHAI SATELLITE ENG INST
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