Research on the Trajectory Model for ZY-3
The new generation Chinese high-resolution three-line stereo-mapping satellite Ziyuan 3 (ZY-3) is equipped with three sensors (nadir, backward, and forward views). Its objective is to manufacture the 1 : 50000 topographic map and revise and update the 1 : 25000 topographic map. For the push-broom sa...
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Online Access: | http://dx.doi.org/10.1155/2014/429041 |
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doaj-2c1ff0e955fa471dbdcc5e044eb3a3dd2020-11-25T00:16:04ZengHindawi LimitedThe Scientific World Journal2356-61401537-744X2014-01-01201410.1155/2014/429041429041Research on the Trajectory Model for ZY-3Yifu Chen0Zhong Xie1National Engineering Research Center for Geographic Information System, China University of Geosciences, 388 Lumo Road, Wuhan 0086-430074, ChinaNational Engineering Research Center for Geographic Information System, China University of Geosciences, 388 Lumo Road, Wuhan 0086-430074, ChinaThe new generation Chinese high-resolution three-line stereo-mapping satellite Ziyuan 3 (ZY-3) is equipped with three sensors (nadir, backward, and forward views). Its objective is to manufacture the 1 : 50000 topographic map and revise and update the 1 : 25000 topographic map. For the push-broom satellite, the interpolation accuracy of orbit and attitude determines directly the satellite’s stereo-mapping accuracy and the position accuracy without ground control point. In this study, a new trajectory model is proposed for ZY-3 in this paper, according to researching and analyzing the orbit and attitude of ZY-3. Using the trajectory data set, the correction and accuracy of the new proposed trajectory are validated and compared with the other models, polynomial model (LPM), piecewise polynomial model (PPM), and Lagrange cubic polynomial model (LCPM). Meanwhile, the differential equation is derivate for the bundle block adjustment. Finally, the correction and practicability of piece-point with weight polynomial model for ZY-3 satellite are validated according to the experiment of geometric correction using the ZY-3 image and orbit and attitude data.http://dx.doi.org/10.1155/2014/429041 |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Yifu Chen Zhong Xie |
spellingShingle |
Yifu Chen Zhong Xie Research on the Trajectory Model for ZY-3 The Scientific World Journal |
author_facet |
Yifu Chen Zhong Xie |
author_sort |
Yifu Chen |
title |
Research on the Trajectory Model for ZY-3 |
title_short |
Research on the Trajectory Model for ZY-3 |
title_full |
Research on the Trajectory Model for ZY-3 |
title_fullStr |
Research on the Trajectory Model for ZY-3 |
title_full_unstemmed |
Research on the Trajectory Model for ZY-3 |
title_sort |
research on the trajectory model for zy-3 |
publisher |
Hindawi Limited |
series |
The Scientific World Journal |
issn |
2356-6140 1537-744X |
publishDate |
2014-01-01 |
description |
The new generation Chinese high-resolution three-line stereo-mapping satellite Ziyuan 3 (ZY-3) is equipped with three sensors (nadir, backward, and forward views). Its objective is to manufacture the 1 : 50000 topographic map and revise and update the 1 : 25000 topographic map. For the push-broom satellite, the interpolation accuracy of orbit and attitude determines directly the satellite’s stereo-mapping accuracy and the position accuracy without ground control point. In this study, a new trajectory model is proposed for ZY-3 in this paper, according to researching and analyzing the orbit and attitude of ZY-3. Using the trajectory data set, the correction and accuracy of the new proposed trajectory are validated and compared with the other models, polynomial model (LPM), piecewise polynomial model (PPM), and Lagrange cubic polynomial model (LCPM). Meanwhile, the differential equation is derivate for the bundle block adjustment. Finally, the correction and practicability of piece-point with weight polynomial model for ZY-3 satellite are validated according to the experiment of geometric correction using the ZY-3 image and orbit and attitude data. |
url |
http://dx.doi.org/10.1155/2014/429041 |
work_keys_str_mv |
AT yifuchen researchonthetrajectorymodelforzy3 AT zhongxie researchonthetrajectorymodelforzy3 |
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