Abstract

The star image suffers inevitably from degradation due to the high-speed motion of the space target and the long exposure time of the camera, therefore the attitude information of the star is hard to accurately obtain. This paper proposes a blind deblurring algorithm that combines shape features of space targets. First, the astronomical image is preprocessed using saliency detection. Then, considering the shape characteristics of space targets, the Minimum Bounding Rectangle (MBR) is introduced to describe the space targets. Next, the parameters of the MBR are used to estimate the point spread function (PSF). Finally, a regularization method is employed to recover the astronomical images. Experimental results on both simulation and real star images demonstrate that the proposed method reduces the error of point spread function estimation and decreases the error rate of identified space targets. At the same time, the accuracy of the star centroid extraction improves 0.2786 on average and the error of the star centroid location extraction reduces 0.059 comparing to the state-of-art method. The proposed method is of great significance for positioning, recognition and attitude determination of space targets.

Highlights

  • With the further study of human beings in the field of deep space exploration, the quality requirements for star images are getting higher and higher

  • The detection of the Middle Earth Orbit (MEO) space targets is mainly achieved by ground-based optoelectronic telescopes with star sensors [2], [3]

  • The space target is identified using Minimum Bounding Rectangle (MBR) and the point spread function is estimated based on motion length estimation and motion angle estimation

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Summary

Introduction

With the further study of human beings in the field of deep space exploration, the quality requirements for star images are getting higher and higher. Since most of the targets are passive, passive detection equipment is widely used for observation. The detection of the Middle Earth Orbit (MEO) space targets is mainly achieved by ground-based optoelectronic telescopes with star sensors [2], [3]. A star tracker, known as star sensor, is a high-precision, autonomous attitude measurement device, which can carry out attitude estimation without prior information and does not drift with time. It is widely used in various types of spacecraft [4]

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