Orbital and attitude cooperative control of small satellite in proximity operation

Yanzhao Zhang; Jianping Yuan; Jianjun Luo; Wenyong Zhou

Orbital and attitude cooperative control of small satellite in proximity operation

Yanzhao Zhang
, Jianping Yuan
, Jianjun Luo
, Wenyong Zhou

航天学院

Northwestern Polytechnical University Xian

科研成果: 期刊稿件 › 文章 › 同行评审

1 引用（Scopus）

摘要

Positional and attitude error dynamics model of small satellite relative to a target satellite was derived, then the desired relative orbit and desired attitude of small satellite were designed. Orbital and attitude cooperative control strategy was used and the parametric uncertainty of small satellite was considered. An adaptive full-state feedback controller was designed. Numerical simulation shows the controller is adaptive well.

源语言	英语
页（从-至）	13-19
页数	7
期刊	Zhongguo Kongjian Kexue Jishu/Chinese Space Science and Technology
卷	28
期	5
出版状态	已出版 - 10月 2008

其它文件与链接

链接到 Scopus 的出版物

引用此

@article{e0f891259fd84abc9ec227795bd6b6dc,

title = "Orbital and attitude cooperative control of small satellite in proximity operation",

abstract = "Positional and attitude error dynamics model of small satellite relative to a target satellite was derived, then the desired relative orbit and desired attitude of small satellite were designed. Orbital and attitude cooperative control strategy was used and the parametric uncertainty of small satellite was considered. An adaptive full-state feedback controller was designed. Numerical simulation shows the controller is adaptive well.",

keywords = "Adaptive control, Attitude tracking, Orbital and attitude cooperative control, Proximity operation, Small satellite",

author = "Yanzhao Zhang and Jianping Yuan and Jianjun Luo and Wenyong Zhou",

year = "2008",

month = oct,

language = "英语",

volume = "28",

pages = "13--19",

journal = "Zhongguo Kongjian Kexue Jishu/Chinese Space Science and Technology",

issn = "1000-758X",

publisher = "Chinese Academy of Space Technology",

number = "5",

}

TY - JOUR

T1 - Orbital and attitude cooperative control of small satellite in proximity operation

AU - Zhang, Yanzhao

AU - Yuan, Jianping

AU - Luo, Jianjun

AU - Zhou, Wenyong

PY - 2008/10

Y1 - 2008/10

N2 - Positional and attitude error dynamics model of small satellite relative to a target satellite was derived, then the desired relative orbit and desired attitude of small satellite were designed. Orbital and attitude cooperative control strategy was used and the parametric uncertainty of small satellite was considered. An adaptive full-state feedback controller was designed. Numerical simulation shows the controller is adaptive well.

AB - Positional and attitude error dynamics model of small satellite relative to a target satellite was derived, then the desired relative orbit and desired attitude of small satellite were designed. Orbital and attitude cooperative control strategy was used and the parametric uncertainty of small satellite was considered. An adaptive full-state feedback controller was designed. Numerical simulation shows the controller is adaptive well.

KW - Adaptive control

KW - Attitude tracking

KW - Orbital and attitude cooperative control

KW - Proximity operation

KW - Small satellite

UR - https://www.scopus.com/pages/publications/58149218005

M3 - 文章

AN - SCOPUS:58149218005

SN - 1000-758X

VL - 28

SP - 13

EP - 19

JO - Zhongguo Kongjian Kexue Jishu/Chinese Space Science and Technology

JF - Zhongguo Kongjian Kexue Jishu/Chinese Space Science and Technology

IS - 5

ER -

Orbital and attitude cooperative control of small satellite in proximity operation

摘要

其它文件与链接

指纹

引用此