On orbit estimation of spacecraft dynamic property
ZhaoYang, ZHANG Da-wei, Tian Hao, 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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On orbit estimation of spacecraft dynamic property
本站小编 哈尔滨工业大学/2019-10-23
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