Optical system for star sensor

An optical system and star sensor technology, which is applied in the optical system for star sensors and in the field of optical engineering, can solve the problem of difficult processing of aspheric optical systems, low pass rate of aspheric lens parts, unfavorable light weight of star sensors, etc. problems, to achieve good space thermal stability, good space environment adaptability, and improve the effect of attitude measurement accuracy
CN104833355AActive Publication Date: 2015-08-12BEIJING INST OF CONTROL ENG
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
BEIJING INST OF CONTROL ENG
Publication Date
2015-08-12

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Abstract

The invention relates to an optical system for a star sensor. The optical system is applied to high-precision star sensors. The optical system is of an improved peaceful structure and consists of six lenses, wherein the six lenses are all spherical lenses; an aperture diaphragm is arranged on first glass; the first glass is made of fused quartz, can be used for correcting aberration and can be used as protective glass of the optical system. The optical system has the characteristics of wide spectrum, large visual field, relative large aperture and the like; the distortion is very low in relatively large spectral range and visual fields, concentration ratios of discs of confusion of each visual field are uniformly distributed, and the imaging quality is good. The optical system can work in a temperature range from -40 DEG C to 50 DEG C, has good image quality and defocusing amount at each temperature point and can meet attitude measurement requirements of the high-precision star sensors working at severe space temperature environments.
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Description

Technical field

[0001] The invention relates to an optical system for a star sensor, which belongs to the category of optical engineering. Background technique

[0002] The invention is used in a star sensor for spacecraft. The star sensor uses the star as the measurement target. The star is imaged on the photoelectric converter through the optical system. The output signal is sent to the data processing unit through A / D conversion. After star point extraction and star map recognition, the optical axis vector of the star sensor is determined The pointing in the inertial coordinate system determines its three-axis attitude in the inertial coordinate system through the installation matrix of the star sensor on the aircraft, the starlight navigation system and the ship.

[0003] The star sensor is generally composed of a light shield, an optical system, a detector component and its circuit, a data processing circuit, a secondary power supply, software (system software, application so...

Claims

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