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Miniaturized radar dynamic attitude measurement equipment

A dynamic and equipment technology, which is applied in the directions of measuring devices, measuring angles, surveying and navigation, etc., to achieve the effect of high attitude measurement accuracy, small size and good dynamic performance

Pending Publication Date: 2022-06-10
BEIJING INST OF SPACE LAUNCH TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003]At present, the attitude measuring equipment on the market is mainly based on the spirit level, which can provide high attitude accuracy under static conditions, but in actual working conditions, the radar front Affected by many factors such as wind blowing, radar rotation, and road sinking, the front is in a shaking state for a long time, and the static level does not meet the needs of actual combat.

Method used

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  • Miniaturized radar dynamic attitude measurement equipment
  • Miniaturized radar dynamic attitude measurement equipment
  • Miniaturized radar dynamic attitude measurement equipment

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Embodiment Construction

[0022] Exemplary embodiments of the present disclosure will be described in more detail below with reference to the accompanying drawings. Although exemplary embodiments of the present disclosure are shown in the drawings, it should be understood that the present disclosure may be embodied in various forms and should not be limited by the embodiments set forth herein. Rather, these embodiments are provided for more thorough understanding of the present disclosure and to fully convey the scope of the present disclosure to those skilled in the art.

[0023] The following combination Figure 1 to Figure 3 , to illustrate the miniaturized radar dynamic attitude measurement equipment provided by the embodiment of the present invention, see figure 1 and image 3 , The miniaturized radar dynamic attitude measurement device provided by the embodiment of the present invention includes: a box body 1, and a fiber optic gyro combination 2, an accelerometer 3, an IF board 4, a main contr...

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Abstract

The invention provides miniaturized radar dynamic attitude measurement equipment, which comprises a box body 1, and a fiber-optic gyroscope combination 2, an accelerometer 3, an IF plate 4, a main control board 5 and a power supply module 6 which are arranged in the box body 1, wherein the fiber-optic gyroscope combination 2 is used for measuring triaxial angular rate data in real time; the accelerometer 3 is used for measuring acceleration data in a carrier movement process, converting an accelerometer signal into a current signal, outputting the current signal to the IF board 4, converting the current signal output by the accelerometer into a pulse signal, and outputting the pulse signal to the main control board 5; the main control board 5 is used for receiving and collecting triaxial angular rate data measured by the fiber-optic gyroscope combination 2 and acceleration data measured by the accelerometer 3, and carrying out dynamic attitude measurement; the power supply module 6 is used for converting an input direct-current power supply into a power supply required by each component in the product; and the main control board 5 is specifically used for carrying out attitude correction on triaxial angular rate data measured by the fiber-optic gyroscope combination 2 and acceleration data measured by the accelerometer 3 through a complementary filter to obtain attitude information.

Description

technical field [0001] The invention relates to the technical field of attitude measurement, in particular to a miniaturized radar dynamic attitude measurement device. Background technique [0002] Radar is the "eye" of the weapon system and an important source of information in the combat system. It is responsible for the important tasks of discovery, tracking, identification, guidance, and indicator lights. The detection accuracy of the radar directly affects the combat effectiveness and survivability of the weapon system. Improving the real-time attitude measurement accuracy of the radar front is an important means to ensure the detection accuracy of the radar. [0003] At present, the attitude measuring equipment on the market is mainly based on the spirit level, which can provide high attitude accuracy under static conditions, but in actual working conditions, the radar front is affected by many factors such as wind blowing, radar rotation, and road surface sinking. Th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01C1/00G06K9/00
CPCG01C1/00G06F2218/02G06F2218/04
Inventor 李旬焦晨阳张靖李朝阳王盛余胜义王庆广余海敏
Owner BEIJING INST OF SPACE LAUNCH TECH
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