Method for testing porthole-type star sensor system

A technology of system testing and testing method, applied in the direction of measuring devices, instruments, etc., can solve the problem of not considering the influence of the porthole on the attitude determination ability of the star sensor, which is not conducive to the attitude determination of the star sensor, and cannot verify whether the porthole star sensor is not. Satisfy task requirements, etc.

Active Publication Date: 2017-07-14
SHANGHAI AEROSPACE CONTROL TECH INST
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AI Technical Summary

Problems solved by technology

Because glass has optical properties such as reflection, refraction, and scattering, it may have some impact on the function and performance of the star sensor
When the star sensor determines the attitude, it needs to extract the star point information from the shooting star map. The starlight falls on the star sensitive detector after being refracted by the porthole glass, which may affect the star point energy and the angular distance between the stars reaching the detector, and then affect the starlight. Attitude measurement accuracy of the sensor
When there is external light (such as sunlight, moonlight), the glass may change the optical path and generate new stray light, which increases the background gray threshold of the captured star map, which is not conducive to the star sensor to extract star point information for attitude determination
The existing star sensor testing technology only tests the star sensor, without considering the influence of portholes on the attitude determination ability of the star sensor; and this method is the first application in China, and there is no corresponding use experience for reference
If the porthole-type star sensor is not systematically tested to find out the possible impact of the porthole on the detection sensitivity, measurement accuracy and stray light of the star sensor, it will be impossible to verify whether the porthole-type star sensor meets the mission requirements, and the use strategy requires Matters needing attention

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  • Method for testing porthole-type star sensor system
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  • Method for testing porthole-type star sensor system

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Embodiment Construction

[0049] Such as Figure 4 Shown is a flow chart of the present invention, further illustrating specific embodiments of the present invention.

[0050] (1) Single star model accuracy test

[0051] a) Installation and alignment: as figure 1 As shown, adjust the optical axis of the single-star simulator to be horizontal and point to the center of gyration of the turntable. The optical axis of the single-star simulator is perpendicular to the plane determined by the rotary axis of the inner frame and the outer frame of the turntable; the star sensor is installed on the mounting surface of the inner frame of the turntable, and the parallel light emitted by the single-star simulator is incident on the principal point along the optical axis. The initial alignment accuracy of the single star simulator and star sensor, star sensor and turntable is guaranteed by photoelectric autocollimator. Place the porthole optical axis parallel to the star sensitive optical axis.

[0052] b) Test...

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Abstract

The invention discloses a method for testing a porthole-type star sensor system. The method comprises (1) carrying out a porthole-type star sensor static precision test through a single star simulator, (2) comparing the influence caused by a porthole on star sensor detection sensitivity through star sensor picture photographing under the actual sky background, (3) aligning a star sensor having a porthole to a sky area, carrying out continuous working for some time and carrying out statistics on static measuring accuracy, (4) putting the star sensor on a rotary table, carrying out rotation at a certain angle rate and measuring influence caused by the porthole on dynamic tracking performances of the star sensor, and (5) testing the influence caused by the porthole on a stray light protection angle through a solar simulator. The invention provides the method for testing a porthole-type star sensor system for the first time. The method can test the influence caused by the porthole on star sensor functions and performance indexes, can verify whether the design satisfies system task demands, is conducive to specific design improvement of the porthole-type star sensor and provides guidance for on-orbit use strategy of a porthole-type star sensor.

Description

technical field [0001] The invention relates to the technical field of satellite stand-alone testing, in particular to a testing method for a porthole-type star sensor system. Background technique [0002] Ordinary star sensor attitude measurement often adopts the method of directly shooting star maps for attitude determination; due to mission application requirements, the star sensor is installed inside the aircraft, and the attitude is determined through the porthole. In order to ensure that the star sensor can take star maps normally, the portholes are made of glass with high light transmittance. Because glass has optical properties such as reflection, refraction, and scattering, it may have certain effects on the function and performance of the star sensor. When the star sensor determines the attitude, it needs to extract the star point information from the shooting star map. The starlight falls on the star sensitive detector after being refracted by the porthole glass,...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01C25/00
CPCG01C25/00
Inventor 王向郭旭升施常勇张召弟艾奇
Owner SHANGHAI AEROSPACE CONTROL TECH INST
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