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空间目标轨道预报及望远镜观测实现
引用本文:王若璞,郑勇,鲁强.空间目标轨道预报及望远镜观测实现[J].海洋测绘,2010,30(1):35-37.
作者姓名:王若璞  郑勇  鲁强
作者单位:1. 解放军信息工程大学,测绘学院,河南,郑州,450052
2. 海军海洋测绘研究所,天津,300061
摘    要:分析了空间目标两行轨道根数(TLE)的格式及构成;阐述了相应的SGP4/SDP4轨道近似解析模型算法;提供了轨道坐标系与J2000.0坐标系及观测地平坐标系之间的转换关系。研究了ASCOM控件的用法,并结合TLE数据计算结果编程实现了用Meade望远镜对空间目标的自动搜索与跟踪观测。

关 键 词:空间目标  两行轨道根数  SGP4/SDP4模型  ASCOM控件  望远镜

Space Object Orbital Prediction and Telescope Observation
WANG Ruo-pu,ZHENG Yong,LU Qiang.Space Object Orbital Prediction and Telescope Observation[J].Hydrographic Surveying and Charting,2010,30(1):35-37.
Authors:WANG Ruo-pu  ZHENG Yong  LU Qiang
Institution:1.Institute of Surveying and Mapping;Information Engineering University;Zhengzhou;Henan;450052;2.Naval Institute of Hydrographic Surveying and Charting;Tianjin;300061
Abstract:The format and composition of two-line element sets were analyzed firstly.And then Simplified General Perturbations Version 4 and Simplified Deep-space Perturbation(SGP4/SDP4) orbital model which developed from analytic orbital theory were introduced.And the coordinate transformation from True Equator and Mean Equinox of Date to J2000.0 and to topocentric-horizon system was provided.Space object observation software based on TLE and ASCOM control with Meade telescope was developed.
Keywords:space object  TLE  SGP4/SDP4 model  ASCOM control  telescope  
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