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| 引用本文： | 李谦,何正斌.���Ǹ��پ�γ�ǵ���ת��ģ��ת���Ծ����㷨�о�[J].大地测量与地球动力学,2015,35(1):172-176. |
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| 作者姓名： | 李谦 何正斌 |
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| 作者单位： | 中国测绘科学研究院， 北京市莲花池西路28号， 100830 |
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| 摘 要： | ???????????γ?????????????????????????????????????????γ??????????????????????????滮??γ????????????????????????豸??????????????????γ???????????“??????/??λ???”??????????????ε???????????????????????????????????????????????????γ???
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| 关 键 词： | ??γ?? ????? ??? ???????? |
| 收稿时间： | 2013-01-13 |
Research on Modeling and Automated Planning of Rotation Trajectory of Satellite Tracking Theodolite |
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| LI Qian,HE Zhengbin.Research on Modeling and Automated Planning of Rotation Trajectory of Satellite Tracking Theodolite[J].Journal of Geodesy and Geodynamics,2015,35(1):172-176. |
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| Authors: | LI Qian HE Zhengbin |
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| Institution: | Chinese Academy of Surveying and Mapping, 28 West-Lianluachi Road, Beijing 100830， China |
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| Abstract: | This paper proposes a method of modeling the rotation trajectory of satellite tracking theodolite and puts forward an algorithm which can make automated planning about the rotation trajectory of the theodolite on the basis of the satellite’s trajectory and the theodolite’s historical trajectory. This algorithm plans the rotation trajectory in advance which can keep the hardware safe and at the same time avoid the lost of observation arcs owing to the situations when the rotation is limited and the theodolite has to reverse or motor’s power was shut down and the theodolite has to be pushed back. This algorithm can be applied to the SLR theodolite and others tracking the satellite. |
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| Keywords: | theodolite rotation trajectory modeling self-decision of rotation trajectory |
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