DocumentCode
3047242
Title
The correction of spaceborne satellite´s yaw steering law based on the star tracker high-precision measurement
Author
Yingmei, Sun ; Junli, Chen ; Xiangcheng, Wan ; Ling, Zhang Jiu ; Yun, Wang
Author_Institution
Shanghai Inst. of Satellite Eng., Shanghai, China
fYear
2010
fDate
8-10 June 2010
Firstpage
178
Lastpage
180
Abstract
This paper presents a successful example of how the yaw steering law used in the satellite project. Otherwise in the synthetic aperture radar satellite, the theoretic parameter of the yaw steering law can be obtained and optimized on the track, then the expected Doppler centroid will be gotten.
Keywords
artificial satellites; spaceborne radar; star trackers; synthetic aperture radar; Doppler centroid; satellite project; spaceborne satellite; star tracker high-precision measurement; synthetic aperture radar satellite; yaw steering law; Control systems; Doppler effect; Earth; Orbits; Satellites; Spaceborne radar; Synthetic aperture radar; Doppler centroid; yaw steering law synthetic aperture radar;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
Conference_Location
Harbin
Print_ISBN
978-1-4244-6043-4
Electronic_ISBN
978-1-4244-7505-6
Type
conf
DOI
10.1109/ISSCAA.2010.5633474
Filename
5633474
Link To Document