The kalman filter design for orbiter rendezvous with a non-cooperative target

Qiu Hua Zhang; Ze Cui; Yi Sun

The kalman filter design for orbiter rendezvous with a non-cooperative target

Qiu Hua Zhang^*
, Ze Cui
, Yi Sun

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology

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

Abstract

Considering the request of spacecraft's automatic rendezvous and docking with a non-cooperative target, a method of estimating the motional state based on Kalman filter is investigated. C-W equation is used to modeling the relative motion between satellites. In the case that a radar is taken as the measuring facility, the measurement equation is deduced. Autonomous determination of the relative orbit using extended Kalman filter is addressed. The simulation shows the effectiveness of the method and the influence of system yawp and sampling time to filter.

Original language	English
Pages (from-to)	202-206
Number of pages	5
Journal	Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology
Volume	39
Issue number	SUPPL. 1
State	Published - Jun 2007

Keywords

Automatic rendezvous and docking
Kalman filter
Non-cooperative target
State estimating

Cite this

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title = "The kalman filter design for orbiter rendezvous with a non-cooperative target",

abstract = "Considering the request of spacecraft's automatic rendezvous and docking with a non-cooperative target, a method of estimating the motional state based on Kalman filter is investigated. C-W equation is used to modeling the relative motion between satellites. In the case that a radar is taken as the measuring facility, the measurement equation is deduced. Autonomous determination of the relative orbit using extended Kalman filter is addressed. The simulation shows the effectiveness of the method and the influence of system yawp and sampling time to filter.",

keywords = "Automatic rendezvous and docking, Kalman filter, Non-cooperative target, State estimating",

author = "Zhang, \{Qiu Hua\} and Ze Cui and Yi Sun",

year = "2007",

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pages = "202--206",

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T1 - The kalman filter design for orbiter rendezvous with a non-cooperative target

AU - Zhang, Qiu Hua

AU - Cui, Ze

AU - Sun, Yi

PY - 2007/6

Y1 - 2007/6

N2 - Considering the request of spacecraft's automatic rendezvous and docking with a non-cooperative target, a method of estimating the motional state based on Kalman filter is investigated. C-W equation is used to modeling the relative motion between satellites. In the case that a radar is taken as the measuring facility, the measurement equation is deduced. Autonomous determination of the relative orbit using extended Kalman filter is addressed. The simulation shows the effectiveness of the method and the influence of system yawp and sampling time to filter.

AB - Considering the request of spacecraft's automatic rendezvous and docking with a non-cooperative target, a method of estimating the motional state based on Kalman filter is investigated. C-W equation is used to modeling the relative motion between satellites. In the case that a radar is taken as the measuring facility, the measurement equation is deduced. Autonomous determination of the relative orbit using extended Kalman filter is addressed. The simulation shows the effectiveness of the method and the influence of system yawp and sampling time to filter.

KW - Automatic rendezvous and docking

KW - Kalman filter

KW - Non-cooperative target

KW - State estimating

UR - https://www.scopus.com/pages/publications/36549043030

M3 - 文章

AN - SCOPUS:36549043030

SN - 0367-6234

VL - 39

SP - 202

EP - 206

JO - Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology

JF - Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology

IS - SUPPL. 1

ER -

The kalman filter design for orbiter rendezvous with a non-cooperative target

Abstract

Keywords

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