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An on-orbit autonomous management system and method for a satellite energy system

An autonomous management and energy system technology, applied in the aerospace field, can solve the problems of missing the best time to deal with failures, endangering the safety of the whole satellite, increasing losses, etc., to achieve the effect of on-orbit autonomous maintenance and improve operating life.

Active Publication Date: 2022-02-15
INNOVATION ACAD FOR MICROSATELLITES OF CAS +1
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

In addition, due to the geographical limitation of the ground measurement and control station, it is impossible for the ground station to track the satellite in real time in most cases. If the energy system fails in an unmeasurable arc, if measures are not taken in time, the best treatment for the failure may be missed. Timing will eventually lead to the spread of faults, increased losses, and may even endanger the safety of the entire star

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  • An on-orbit autonomous management system and method for a satellite energy system
  • An on-orbit autonomous management system and method for a satellite energy system
  • An on-orbit autonomous management system and method for a satellite energy system

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[0044] In the following description, the present invention is described with reference to various examples. One skilled in the art will recognize, however, that the various embodiments may be practiced without one or more of the specific details, or with other alternative and / or additional methods, materials, or components. In other instances, well-known structures, materials, or operations are not shown or described in detail so as not to obscure the inventive concepts of the present invention. Similarly, for purposes of explanation, specific quantities, materials and configurations are set forth in order to provide a thorough understanding of embodiments of the invention. However, the invention is not limited to these specific details. Furthermore, it should be understood that the embodiments shown in the drawings are illustrative representations and are not necessarily drawn to correct scale.

[0045] In this specification, reference to "one embodiment" or "the embodiment...

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Abstract

The invention discloses an on-orbit autonomous management system of a satellite energy system, which includes multiple sets of independently working lower computer modules working in a cold backup mode, multiple sets of independently working discharge regulation circuits and charge regulation circuits connected to batteries, and a control center . Wherein, the discharge regulation circuit works in the hot backup mode, and the charge regulation circuit works in the cold backup mode. The state of enabling the autonomous operation of the power controller, the state of autonomous management of the charge and discharge power regulation unit, and the state of autonomous power-on of the accidental protection of charge and discharge are enabled. Fault and fault type, and then according to the fault type, execute the corresponding preset command for autonomous recovery.

Description

technical field [0001] The invention relates to the field of aerospace technology, in particular to an on-orbit autonomous management system and method of a satellite energy system. Background technique [0002] The satellite energy system mainly refers to the generation, change, adjustment and distribution of electric energy, and provides a primary power supply that meets the technical requirements. As an important part of the satellite, it undertakes the task of power supply and distribution for the entire star. The safe and reliable operation of the energy system is an important guarantee for the normal operation of the satellite, and plays a decisive role in improving the performance of the satellite and enhancing the service life of the satellite in orbit. According to the statistical data of spacecraft on-orbit operation failures published at home and abroad in recent years, the energy system has a higher probability of on-orbit failure than other subsystems, and it is...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H02J7/00G01S19/23
CPCH02J7/0047H02J7/007H02J7/0029
Inventor 习成献孔陈杰张强王学良林宝军沈苑何盼陈天明李锐石龙龙王正凯吴敏
Owner INNOVATION ACAD FOR MICROSATELLITES OF CAS