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Portable test launch control device suitable for spacecraft

A technology for measuring, launching, controlling, and spacecraft, applied in the aerospace field, can solve problems such as low integration, poor compatibility and versatility, and achieve the effect of convenient and rapid development, highlighting reusability and versatility

Inactive Publication Date: 2020-12-01
THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0005] The embodiment of the present application provides a portable measurement and control device suitable for spacecraft to solve the problems of low integration, poor compatibility and versatility of the portable measurement and control device in the related art

Method used

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  • Portable test launch control device suitable for spacecraft
  • Portable test launch control device suitable for spacecraft
  • Portable test launch control device suitable for spacecraft

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Embodiment Construction

[0032] In order to make the purposes, technical solutions and advantages of the embodiments of the present application clearer, the technical solutions in the embodiments of the present application will be clearly and completely described below in conjunction with the drawings in the embodiments of the present application. Obviously, the described embodiments It is a part of the embodiments of this application, but not all of them. Based on the embodiments in the present application, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present application.

[0033] see figure 1 As shown, the embodiment of the present application provides a portable measurement, launch and control device suitable for spacecraft, which includes a human-computer interaction device, a main control board, and a measurement and control board. The human-computer interaction device is used to send the operation in...

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Abstract

The invention relates to a portable test launch control device suitable for a spacecraft, and relates to the technical field of spaceflight. The device comprises a man-machine interaction device, a main control board card and a measurement and control board card, the man-machine interaction device is used for sending an operation instruction input by an operator, test launch control software is configured on the main control board card, the test launch control software is provided with multiple control modules, and the control modules are used for receiving the operation instruction; the measurement and control board card is connected with the main control board card and the spacecraft; the measurement and control board card is used for receiving a control instruction issued by each control module according to the operation instruction and controlling the spacecraft to execute a corresponding action, and is further used for receiving feedback signals of the spacecraft, packaging the feedback signals and transmitting the feedback signals to the main control board card; and the man-machine interaction device is used for displaying the spacecraft state obtained according to the feedback signals. The portable test launch control device provided by the invention has outstanding reusability and universality.

Description

technical field [0001] The present application relates to the field of spaceflight technology, in particular to a portable measurement, launch and control device suitable for spacecraft. Background technique [0002] At present, the ground test and launch control system (referred to as the test and launch control system) is used for power supply and distribution control, switching and analog signal measurement of spacecraft and other spacecraft during the ground test and launch stages, and for communication with the control system on the spacecraft. stand-alone communication. [0003] In the existing measurement, launch and control systems, most single machines and combinations adopt centralized control and power distribution. The system is relatively complex, and there are a large number of cables. There are also disadvantages such as long recovery time for the measurement, launch and control system, heavy work for system recovery, more on-site technical support personnel,...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B23/02B64G5/00B64G7/00
CPCB64G5/00B64G7/00G05B23/0213
Inventor 张少雷陈芳张红宋长哲丁波王欢
Owner THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD
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