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Supervised by Ministry of Industry and Information Technology of The People's Republic of China Sponsored by Harbin Institute of Technology Editor-in-chief Yu Zhou ISSNISSN 1005-9113 CNCN 23-1378/T

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Related citation:TIAN Ji-chao,CuiNaiGang,YaoJie,Guo Ji Fong.A stealthy method to determine the relative position and velocity for satellite formation flying[J].Journal of Harbin Institute Of Technology(New Series),2010,17(1):137-140.DOI:10.11916/j.issn.1005-9113.2010.01.026.
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A stealthy method to determine the relative position and velocity for satellite formation flying
Author NameAffiliation
TIAN Ji-chao Dept.of Astronautical Engineering, Harbin Institute of Technology, Harbin 150001,China 
CuiNaiGang Dept.of Astronautical Engineering, Harbin Institute of Technology, Harbin 150001,China 
YaoJie Dept.of Astronautical Engineering, Harbin Institute of Technology, Harbin 150001,China 
Guo Ji Fong Dept.of Astronautical Engineering, Harbin Institute of Technology, Harbin 150001,China 
Abstract:
To achieve the satellite formation control and the succeed formation missions, we present a new stealthy method to determine the relative states between formation satellites. In this method, the combination of a CCD camera and laser radar is used as the relative measure sensors. To reduce electromagnetic radiation, the laser radar works intermittently to minimize the probability of being discovered. And an unscented Kalman filter (UKF) is applied to estimate the relative states. The observability of this method is analyzed. The validity and effectiveness of the method is demonstrated in a typical application of formation relative navigation.
Key words:  formation flying  unscented Kalman filter  relative position and velocity
DOI：10.11916/j.issn.1005-9113.2010.01.026
Clc Number:V249
Fund:

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