Reconfigurable Control System of Secondary Power Supply Failure Switching Unit of Satellite Electronic Products

A secondary power conversion and fault switching technology, applied in the field of control systems, can solve problems such as non-recoverable faults and fault expansion

Active Publication Date: 2021-05-11
SHANGHAI SATELLITE ENG INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The main conversion means of the secondary power supply of satellite electronic products is to use DC / DC to convert the primary and secondary power supplies. As a single-event sensitive device, it is easy to be affected by the space environment or load fluctuations during operation, causing a certain degree of fault. Some faults are recoverable to the DC / DC device itself, and some faults are unrecoverable. When the fault stress accumulates to To a certain extent, it will also cause the expansion of the fault

Method used

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  • Reconfigurable Control System of Secondary Power Supply Failure Switching Unit of Satellite Electronic Products

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Embodiment Construction

[0015] The preferred embodiments of the present invention are given below in conjunction with the accompanying drawings to describe the technical solution of the present invention in detail.

[0016] Such as figure 1 As shown, the control system of the reconfigurable satellite electronic product secondary power supply failure switching unit of the present invention includes a monitoring and control unit, a secondary power supply conversion unit, and a failure switching unit, wherein:

[0017] The monitoring and control unit is connected to the failover unit, which includes a measurement and control information processor, an instruction driver, a telemetry information processing module, and a communication interface. The communication interface is connected to the measurement and control information processor, and the measurement and control information processor is connected to the instruction driver. The module is connected with the measurement and control information process...

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Abstract

The invention discloses a reconfigurable control system for a secondary power supply failure switching unit of satellite electronic products, which includes a monitoring and control unit, a secondary power supply conversion unit, and a failure switching unit, wherein: the monitoring and control unit is connected with the failure switching unit The unit is connected, which includes a measurement and control information processor, an instruction driver, a telemetry information processing module, and a communication interface. The communication interface is connected to the measurement and control information processor, the measurement and control information processor is connected to the instruction driver, and the telemetry information processing module is connected to the measurement and control information processor. . The present invention is based on fault screening and isolation, and a functionally reconfigurable product secondary power distribution system, which can realize the highly reliable design of the secondary power supply of on-board electronic equipment.

Description

technical field [0001] The invention relates to a control system, in particular to a reconfigurable control system for a secondary power supply failure switching unit of satellite electronic products. Background technique [0002] With the development of satellite technology, the stand-alone satellite platform is developing in the direction of integration, light weight, and miniaturization. Various functions of the platform include: power supply and distribution, thermal control, propulsion, measurement and control, SADA mechanism, control of antenna mechanism, etc. Integrated in a few platform integrated electronic stand-alone machines, which are assembled with different functional modules according to functional differences, and provide energy and information interaction services for satellite platform systems. Therefore, the stability of the platform integrated electronic stand-alone Operation and reliability are very important to the whole star. Furthermore, the high rel...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H02J9/06
CPCH02J9/061
Inventor 夏玉林张威铁琳陶震宇陈晓飞李冰
Owner SHANGHAI SATELLITE ENG INST
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