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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Main Authors: Yifu Chen, Zhong Xie
Format: Article
Language:English
Published: Hindawi Limited 2014-01-01
Series:The Scientific World Journal
Online Access:http://dx.doi.org/10.1155/2014/429041
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spelling 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
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AT zhongxie researchonthetrajectorymodelforzy3
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