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Portable measurement and control device for carrier rocket flight control system

A carrier rocket and flight control system technology, applied in the field of portable measurement and control equipment, can solve problems such as unsatisfactory testing, increased cost, and heavy product quality, and achieve the effects of reducing the research and development cycle and risk of research and development, reducing research and development costs, and improving the utilization rate

Inactive Publication Date: 2016-03-30
NO 32 RES INST OF CHINA ELECTRONICS TECH GRP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

This method has been widely used in existing test equipment. This method can also achieve the purpose of multiplexing boards and cards. However, because the data is exchanged through the internal bus, the internal bus protocol chip or Use the method of writing the internal bus protocol inside the FPGA, and at the same time use a common internal bus connector for the versatility of use, resulting in an increase in cost
However, due to the power supply, the quality of the products made is generally very heavy, which cannot meet the purpose of portable testing in the field

Method used

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  • Portable measurement and control device for carrier rocket flight control system

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Embodiment Construction

[0019] 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 modifications and improvements without departing from the concept of the present invention, and these all belong to the protection scope of the present invention.

[0020] figure 1 As shown, the portable measurement and control equipment suitable for the launch vehicle flight control system provided by the present invention, the internal board is a 3U board, and the internal board includes: main control board, each function board and adapter board , various functional boards are connected to the main control board through connectors. Each functional block includes ADC board (including 32-channel AD and 8-channel DA), command acquisition board, 1553B commu...

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PUM

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Abstract

The invention provides a portable measurement and control device for a carrier rocket flight control system. The portable measurement and control device for a carrier rocket flight control system comprises a touch screen and a board card, wherein the board card includes a main control board card, a plurality of function board cards and a transfer board; the plurality of function board cards are connected with the main control board card through a connector; a measurement command is sent to the main control board card through the touch screen; the main control board card converts the measurement command into a corresponding measurement excitation signal; the excitation signal is modulated as a signal which means carrier rocket electronic equipment is available through the signal transfer board; and the carrier rocket electronic equipment performs the corresponding motion. The portable measurement and control device for a carrier rocket flight control system realizes generalization, miniaturization and portability of measurement equipment, and can reduce the cost of the measurement equipment.

Description

technical field [0001] The invention relates to a portable measurement and control device for a flight control system of a launch vehicle, which is suitable for verifying the parameter characteristics of the control system of the launch vehicle during the ground test of each single unit of the control system of the launch vehicle before leaving the factory and before loading the rocket. Background technique [0002] At present, the general test system of the internal bus method is widely used in the ground test system of the domestic launch vehicle before leaving the factory and before loading, which is used for the internal function and performance test of different systems. [0003] The general-purpose test system in the internal bus mode refers to the purpose of testing a variety of different systems through a general-purpose test platform and an additional transfer box between different systems. This method has been widely used in existing test equipment. This method can...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B23/02
CPCG05B23/02
Inventor 郭利民
Owner NO 32 RES INST OF CHINA ELECTRONICS TECH GRP
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