On orbit estimation of spacecraft dynamic property

Yang Zhao; Da Wei Zhang; Hao Tian; Na Li

On orbit estimation of spacecraft dynamic property

Yang Zhao^*
, Da Wei Zhang
, Hao Tian
, Na Li

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology

Research output: Contribution to journal › Article › peer-review

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.

Original language	English
Pages (from-to)	18-22
Number of pages	5
Journal	Journal of Harbin Institute of Technology (New Series)
Volume	18
Issue number	1
State	Published - Feb 2011

Keywords

Estimation
Kalman Filter
Mass property

Cite this

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title = "On orbit estimation of spacecraft dynamic property",

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.",

keywords = "Estimation, Kalman Filter, Mass property",

author = "Yang Zhao and Zhang, \{Da Wei\} and Hao Tian and Na Li",

year = "2011",

month = feb,

language = "英语",

volume = "18",

pages = "18--22",

journal = "Journal of Harbin Institute of Technology (New Series)",

issn = "1005-9113",

publisher = "Harbin Institute of Technology",

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TY - JOUR

T1 - On orbit estimation of spacecraft dynamic property

AU - Zhao, Yang

AU - Zhang, Da Wei

AU - Tian, Hao

AU - Li, Na

PY - 2011/2

Y1 - 2011/2

N2 - 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.

AB - 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.

KW - Estimation

KW - Kalman Filter

KW - Mass property

UR - https://www.scopus.com/pages/publications/79954528174

M3 - 文章

AN - SCOPUS:79954528174

SN - 1005-9113

VL - 18

SP - 18

EP - 22

JO - Journal of Harbin Institute of Technology (New Series)

JF - Journal of Harbin Institute of Technology (New Series)

IS - 1

ER -

On orbit estimation of spacecraft dynamic property

Abstract

Keywords

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