Method and apparatus for testing star sensor function based on electric injection star map

A star sensor and functional testing technology, applied in the direction of measuring devices, machine/structural component testing, instruments, etc., can solve the problems of star field simulators such as high price, poor versatility, and inability to guarantee testing at any time, to achieve testing The method is simple and easy to implement, and the effect of versatility is strong

Inactive Publication Date: 2009-12-23
BEIHANG UNIV
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Problems solved by technology

The disadvantage of this method is that the star field simulator is expensive, and the star field simulator must match the star sensor, and the versatility is not strong
Another commonly used ground function test method is the field star observation test, which is to test under the actual starry sky outdoors. Although this method does not need to simulate the starry sky, it is relatively simple and easy, but it is greatly affected by factors such as weather and cannot Guarantee the demand for testing at any time, and it is impossible to simulate the on-orbit status of the star sensor

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  • Method and apparatus for testing star sensor function based on electric injection star map
  • Method and apparatus for testing star sensor function based on electric injection star map
  • Method and apparatus for testing star sensor function based on electric injection star map

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Embodiment Construction

[0045] The basic idea of ​​the present invention is to provide a test signal source for the star sensor by means of electric injection into the star map, and evaluate the functions of each part of the electronic components of the star sensor by analyzing the processing results, so as to provide a basis for the ground function test of the star sensor A new testing method is provided.

[0046] Here, the so-called electrical injection constellation refers to a digital constellation generated by electrical signal simulation as a test signal source.

[0047] Star sensor function test device such as figure 1 As shown, it consists of a star map simulation computer 1, an information analysis and processing computer 2, a star sensor 3, and a communication cable 4, wherein the star map simulation computer 1 is connected to the star sensor 3 through the communication cable 4, and the star sensor 3 The information analysis and processing computer 2 is connected through a communication c...

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Abstract

The invention discloses a method for testing the function of a star sensor based on an electric injection star map. The method includes: performing simulation calculation on orbital parameters and attitudes of satellite motion, and simulating and generating a star map image captured by the star sensor; Point as the center, update and transmit the local map of the star map; superimpose the local update on the star map background of the star sensor, and perform star point positioning, star map recognition and calculation attitude; check the star map recognition and attitude of the star sensor Whether the result of the solution is correct. The invention also discloses a corresponding device. The star map of the invention has a high update rate, can simulate the on-orbit state of the star sensor, can perform ground simulation experiments together with the whole star system, does not depend on other external equipment, has no special requirements for the use environment, and has strong versatility.

Description

technical field [0001] The invention relates to a star sensor test technology, in particular to a star sensor function test method and device based on an electric injection star map. Background technique [0002] The star sensor is an aerospace measurement instrument that uses star observation to provide high-precision attitude information for space vehicles. Its working principle is: the front-end camera unit of the star sensor uses a charge coupled device (CCD, Charge Coupled Device) The semiconductor (CMOS, Complementary MetalOxide Semiconductor) image sensor captures the star map image, and through the image processing program, the barycenter coordinates and brightness information of the star image point are obtained, and then the star map recognition program uses the obtained information to find the corresponding star in the navigation star library , and finally calculate the three-axis attitude of the star sensor. [0003] Generally, before the star sensor is put into...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01M19/00G01C21/02G01M99/00
Inventor 张广军魏新国刘付成江洁郑循江
Owner BEIHANG UNIV
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