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Star point extraction system and method of star sensor

A technology of star sensor and star point extraction, which is applied in the field of star point extraction system of star sensor, can solve the problems of signal-to-noise ratio reduction, weak star point extraction ability, and less total energy of star points, etc., to improve dynamic Performance, guaranteed star point extraction rate and extraction accuracy

Pending Publication Date: 2021-04-30
SHANGHAI AEROSPACE CONTROL TECH INST
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AI Technical Summary

Problems solved by technology

For the current conventional star point extraction method, the star point extraction is mainly based on the gray threshold of the image and the connected domain as the criterion, and the star point extraction ability is not strong under large dynamic conditions.
The main difficulty is that when the exposure time is long, the "tail" of the star point is too long to easily lead to breakage, and the star point trajectory is divided into several segments, resulting in the failure of the conventional star point extraction method; after shortening the exposure time, the star point can be shortened. Point tailing reduces the possibility of fracture, but it will cause the total energy of the star point received by the detector to decrease, and the signal-to-noise ratio will decrease, making it difficult to extract the star point

Method used

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  • Star point extraction system and method of star sensor

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Embodiment Construction

[0037] The following is attached figure 1 The present invention will be further described in detail with specific embodiments. The advantages and features of the present invention will become clearer from the following description. It should be noted that the drawings are in a very simplified form and all use imprecise scales, which are only used to facilitate and clearly assist the purpose of illustrating the embodiments of the present invention. In order to make the objects, features and advantages of the present invention more comprehensible, please refer to the accompanying drawings. It should be noted that the structures, proportions, sizes, etc. shown in the drawings attached to this specification are only used to match the content disclosed in the specification, for those who are familiar with this technology to understand and read, and are not used to limit the implementation of the present invention. condition, so it has no technical substantive meaning, and any mod...

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Abstract

The invention discloses a star point extraction method of a star sensor. The method comprises the following steps: establishing a star point energy distribution model under a dynamic condition; predicting a current moment coordinate of the star point, and windowing by taking the current moment coordinate of the star point as a center; taking the star point energy distribution model under the dynamic condition as a template, calculating correlation point by point in a window, and taking a region with the maximum correlation as a region where a star point is located; and covering the region where the star point is located by using the star point energy distribution model under a dynamic condition, and calculating the coordinates of the star point by using a gray weighted centroid method. According to the invention, the star sensor dynamic model is used as a template, and the correlation is used as a basis so that the star point extraction rate and extraction precision of the star sensor under a large dynamic condition are ensured, and the dynamic performance of the star sensor is improved.

Description

technical field [0001] The invention relates to space control technology, in particular to a star point extraction system and method for a star sensor. Background technique [0002] The dynamics of the star sensor refers to the ability of the star sensor to adapt to the rotation when the spacecraft rotates at a certain angular velocity, which is an important indicator of the star sensor. Satellites have requirements for the dynamic performance of star sensors in large dynamic situations such as initial orbiting, maneuvering, and large-angle attitude adjustment. More applications of star sensors on high-mobility spacecraft such as space maneuvering platforms and missiles are based on star sensors. Higher requirements are put forward for the dynamic performance. [0003] The difficulties in improving the dynamics of the star sensor are as follows. Since star sensor imaging is a process of energy integration, the energy distribution of its imaging spot (star point) is related...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01C21/02
CPCG01C21/02
Inventor 练达毛晓楠杨元钊任平川王丹娜翟正一刘轩
Owner SHANGHAI AEROSPACE CONTROL TECH INST
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