On-orbit system identification experiments on Engineering Test Satellite-VI

Shuichi Adachi; Isao Yamaguchi; Takashi Kida; Takeshi Sekiguchi; Katsuhiko Yamada; Yuichi Chida

doi:10.1016/s0967-0661(99)00032-5

On-orbit system identification experiments on Engineering Test Satellite-VI

Shuichi Adachi, Isao Yamaguchi, Takashi Kida, Takeshi Sekiguchi, Katsuhiko Yamada, Yuichi Chida

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

31 Citations (Scopus)

Abstract

On-orbit system identification experiments were performed using the Engineering Test Satellite-VI (ETS-VI), launched in 1994. The purpose of the experiments is to check the validity of a mathematical model for ETS-VI which was previously obtained by ground experiments. Two kinds of system identification schemes are utilized. One is a traditional scheme based on polynomial black-box models such as the prediction error method, and the other is a subspace method based on state-space models. The purpose of this paper is to compare these system identification schemes using experimental data. It will be shown that the subspace method proves to be promising for the system identification of large space structures typified by ETS-VI.

Original language	English
Pages (from-to)	831-841
Number of pages	11
Journal	Control Engineering Practice
Volume	7
Issue number	7
DOIs	https://doi.org/10.1016/s0967-0661(99)00032-5
Publication status	Published - 1999 Jul
Externally published	Yes

Keywords

Aerospace
Least-squares method
Prediction error methods
Subspace methods
System identification

ASJC Scopus subject areas

Control and Systems Engineering
Computer Science Applications
Electrical and Electronic Engineering
Applied Mathematics

Access to Document

10.1016/s0967-0661(99)00032-5

Cite this

@article{d32b65bf5244452b8e5411d2aad55bf9,

title = "On-orbit system identification experiments on Engineering Test Satellite-VI",

abstract = "On-orbit system identification experiments were performed using the Engineering Test Satellite-VI (ETS-VI), launched in 1994. The purpose of the experiments is to check the validity of a mathematical model for ETS-VI which was previously obtained by ground experiments. Two kinds of system identification schemes are utilized. One is a traditional scheme based on polynomial black-box models such as the prediction error method, and the other is a subspace method based on state-space models. The purpose of this paper is to compare these system identification schemes using experimental data. It will be shown that the subspace method proves to be promising for the system identification of large space structures typified by ETS-VI.",

keywords = "Aerospace, Least-squares method, Prediction error methods, Subspace methods, System identification",

author = "Shuichi Adachi and Isao Yamaguchi and Takashi Kida and Takeshi Sekiguchi and Katsuhiko Yamada and Yuichi Chida",

year = "1999",

month = jul,

doi = "10.1016/s0967-0661(99)00032-5",

language = "English",

volume = "7",

pages = "831--841",

journal = "Control Engineering Practice",

issn = "0967-0661",

publisher = "Elsevier Limited",

number = "7",

}

TY - JOUR

T1 - On-orbit system identification experiments on Engineering Test Satellite-VI

AU - Adachi, Shuichi

AU - Yamaguchi, Isao

AU - Kida, Takashi

AU - Sekiguchi, Takeshi

AU - Yamada, Katsuhiko

AU - Chida, Yuichi

PY - 1999/7

Y1 - 1999/7

N2 - On-orbit system identification experiments were performed using the Engineering Test Satellite-VI (ETS-VI), launched in 1994. The purpose of the experiments is to check the validity of a mathematical model for ETS-VI which was previously obtained by ground experiments. Two kinds of system identification schemes are utilized. One is a traditional scheme based on polynomial black-box models such as the prediction error method, and the other is a subspace method based on state-space models. The purpose of this paper is to compare these system identification schemes using experimental data. It will be shown that the subspace method proves to be promising for the system identification of large space structures typified by ETS-VI.

AB - On-orbit system identification experiments were performed using the Engineering Test Satellite-VI (ETS-VI), launched in 1994. The purpose of the experiments is to check the validity of a mathematical model for ETS-VI which was previously obtained by ground experiments. Two kinds of system identification schemes are utilized. One is a traditional scheme based on polynomial black-box models such as the prediction error method, and the other is a subspace method based on state-space models. The purpose of this paper is to compare these system identification schemes using experimental data. It will be shown that the subspace method proves to be promising for the system identification of large space structures typified by ETS-VI.

KW - Aerospace

KW - Least-squares method

KW - Prediction error methods

KW - Subspace methods

KW - System identification

UR - http://www.scopus.com/inward/record.url?scp=0032686753&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=0032686753&partnerID=8YFLogxK

U2 - 10.1016/s0967-0661(99)00032-5

DO - 10.1016/s0967-0661(99)00032-5

M3 - Article

AN - SCOPUS:0032686753

SN - 0967-0661

VL - 7

SP - 831

EP - 841

JO - Control Engineering Practice

JF - Control Engineering Practice

IS - 7

ER -

On-orbit system identification experiments on Engineering Test Satellite-VI

Abstract

Keywords

ASJC Scopus subject areas

Access to Document

Other files and links

Fingerprint

Cite this