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Power distribution measurement and control unit for spacecraft

A technology for measurement and control units and spacecraft, applied in general control systems, instruments, simulators, etc., can solve problems such as no explanation or report found, and data not yet collected, so as to shorten the development cycle, reduce the weight of satellite cable networks, and reduce The effect of platform quality

Active Publication Date: 2017-11-07
SHANGHAI SATELLITE ENG INST
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  • Abstract
  • Description
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Problems solved by technology

[0004] At present, there is no description or report of the similar technology of the present invention, and no similar data at home and abroad have been collected yet.

Method used

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  • Power distribution measurement and control unit for spacecraft
  • Power distribution measurement and control unit for spacecraft
  • Power distribution measurement and control unit for spacecraft

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Embodiment Construction

[0034] The following is a detailed description of the embodiments of the present invention: this embodiment is implemented on the premise of the technical solution of the present invention, and provides detailed implementation methods and specific operation processes. 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, and these all belong to the protection scope of the present invention.

[0035] Please also see Figure 1 to Figure 6 .

[0036] This embodiment provides a power distribution measurement and control unit for a spacecraft, including an integrated power supply and distribution module, a remote control module, a telemetry module, and a heater control module, wherein the remote control module is connected to the power supply and distribution module and the heater control module respectively. The controller control module controls the connection, and the power s...

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Abstract

The invention provides a power distribution measuring and control unit for a spacecraft. The power distribution measuring and control unit comprises a power supply and distribution module, a remote control module, a remote measuring module and a heater control module, wherein the power supply and distribution module, the remote control module, the remote measuring module and the heater control module are integrated. The remote control module is in control connection with the power supply and distribution module and the heater control module, and the power supply and distribution module is further connected with the remote measuring module. The power distribution measuring and control unit solves the problems that a platform single-machine product of an existing spacecraft is single in function, low in integration level, and large in size and weight, and more entire satellite resources are occupied. The precondition is provided for design of satellite integration, the good effect in reducing the weight of a satellite cable net is achieved, and meanwhile the development cycle and the development cost of a spacecraft single-machine product can be reduced.

Description

technical field [0001] The invention relates to the technical field of stand-alone product design of spacecraft, in particular to a power distribution measurement and control unit for spacecraft that adopts a modular design mode of a spacecraft stand-alone and has highly integrated functions. Background technique [0002] At present, the functions of satellite power supply and distribution, telemetry, remote control, and heater control are completed by independent stand-alone products, such as power distributors, telemetry samplers, central remote control machines, thermal control control boxes, etc., occupying a large amount of satellite platform resources. [0003] As the complexity of spacecraft products continues to increase and the demand for load capacity further increases, the design of satellite platforms requires weight reduction, functional integration, and high efficiency. The development of integrated platform stand-alone products with integrated management of mu...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B19/042
CPCG05B19/0428
Inventor 张坤夏玉林铁琳陆国平金历群
Owner SHANGHAI SATELLITE ENG INST
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