Detection of attitude constant error and in-orbit calibration for the three-line CCD sensor of the ZY-3 satellite-Reference-Cited by-同舟云学术

Detection of attitude constant error and in-orbit calibration for the three-line CCD sensor of the ZY-3 satellite

Published:2017-09-14 Issue:23 Volume:38 Page:7333-7356
ISSN:0143-1161
Container-title:International Journal of Remote Sensing
language:en
Short-container-title:International Journal of Remote Sensing

Author:

Chen Yifu¹²,Qiu Zhenge³,Xie Zhong²,Le Yuan²,Fang Shenghui⁴

Affiliation:

1. National Engineering Research Center for Geographic Information System, China University of Geosciences (Wuhan), Wuhan, China

2. Facility of Information Engineering, China University of Geosciences (Wuhan), Wuhan, China

3. Key Laboratory of Space Active Opto-electronics Technology, Chinese Academy of Sciences, Shanghai, China

4. Remote Sensing Information Engineering Institute, Wuhan University, Wuhan, China

Funder

The key techniques of marine surveying and mapping based on the domestic high-resolution satellite

Publisher

Informa UK Limited

Subject

General Earth and Planetary Sciences

Link

https://www.tandfonline.com/doi/pdf/10.1080/01431161.2017.1372858

Reference39 articles.

1. Research on the Trajectory Model for ZY-3

2. SENSOR CALIBRATION OF THREE-LINE CCD SCANNERS ON ZY-3

3. Hu, F. 2010. “Research on Inner FOV Stitching Theories and Algorithms for Sub-images of Three Non-collinear TDI CCD Chips.” Ph.D. Dissertation., Federal Institute of Remote sensing, Wuhan, China.

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