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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:ZhaoYang,ZHANG Da-wei,Tian Hao,LiNa.On orbit estimation of spacecraft dynamic property[J].Journal of Harbin Institute Of Technology(New Series),2011,18(1):18-22.DOI:10.11916/j.issn.1005-9113.2011.01.004.
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On orbit estimation of spacecraft dynamic property
Author NameAffiliation
ZhaoYang Dept.of Aerospace Engineering,Harbin Institute of Technology,Harbin 150001,China 
ZHANG Da-wei Dept.of Aerospace Engineering,Harbin Institute of Technology,Harbin 150001,China 
Tian Hao Dept.of Aerospace Engineering,Harbin Institute of Technology,Harbin 150001,China 
LiNa Dept.of Aerospace Engineering,Harbin Institute of Technology,Harbin 150001,China 
Abstract:
Mass property of spacecraft needs to be estimated in certain circumstances.Based on the measurement of single point acceleration,angular acceleration and angular velocity,a discrete Kalman Filter(KF) based estimation method is developed to extract the inertia matrix and mass center.The simulation results show that the method can be used for continues online estimation without propellant consumption.Stability condition for the filter is given at last.
Key words:  mass property  Kalman Filter  estimation
DOI：10.11916/j.issn.1005-9113.2011.01.004
Clc Number:V415.4
Fund:

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