Application of Fuzzy Information Intelligent Computing Theory in Space Target Recognition

Kai Du, Hai-yue Li, Kejuan Xu, Jianping Liu, Jin-Yuan Li, Dan Wang, Jingfeng Sun
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Abstract

In this paper, the fuzzy relative entropy of fuzzy information theory is introduced for the spatial target orbit information and its related characteristics are discussed. For the tens of thousands of spatial target orbital feature information in the space target orbit information database, the J2000 inertial mean orbit elements are used to construct the respective fuzzy feature vectors. The fuzzy relative entropy discriminant algorithm is used to model and analyze the big data information of the target and the orbit information base. After 10 sets of near-ground circular orbits and 6 sets of medium-high orbits to be identified and fuzzy relative entropy recognition calculation of the orbit information database, the proportion of the target to be identified correctly identified as a unique spatial target can reach up to 63%. Due to the influence of the orbital error and the threshold error, the initial identification of the orbit is often as many as several dozen. Compared with the traditional empirical threshold interval recognition technology that relies on the orbit feature information, the method can greatly improve the success rate of the recognition calculation. Since the spatial information of the target orbit feature itself is fuzzy, there is always a deviation from the actual rail orbit calculation. Therefore, the fuzzy relative entropy method is reasonable. The method applies the information discrimination characteristics of fuzzy information theory to measure the spatial target orbit. Compared with the traditional orbit feature information recognition method, it has the characteristics of high computational efficiency, large information discrimination, strong anti-interference performance and high recognition success rate. It has a good application prospect in the field of space target (fragment) detection and identification.
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模糊信息智能计算理论在空间目标识别中的应用
本文将模糊信息理论中的模糊相对熵引入到空间目标轨道信息中,并对其相关特征进行了讨论。针对空间目标轨道信息库中数以万计的空间目标轨道特征信息,采用J2000惯性平均轨道元构建各自的模糊特征向量。采用模糊相对熵判别算法对目标和轨道信息库的大数据信息进行建模和分析。待识别的10组近地圆形轨道和6组中高轨道经过轨道信息库模糊相对熵识别计算后,待识别目标被正确识别为唯一空间目标的比例可达63%。由于轨道误差和阈值误差的影响,初始识别的轨道往往多达几十个。与传统的基于轨道特征信息的经验阈值区间识别技术相比,该方法可以大大提高识别计算的成功率。由于目标轨道特征本身的空间信息是模糊的,与实际轨道计算结果存在一定的偏差。因此,模糊相对熵法是合理的。该方法利用模糊信息理论的信息判别特性对空间目标轨道进行测量。与传统的轨道特征信息识别方法相比,具有计算效率高、信息判别量大、抗干扰性能强、识别成功率高等特点。在空间目标(碎片)检测与识别领域具有良好的应用前景。
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