Quasi-linear model reference tracking control of approaching non-cooperative target based on direct parametric control

Guang Ren Duan; Gang Xu

doi:10.1109/ChiCC.2016.7553810

Quasi-linear model reference tracking control of approaching non-cooperative target based on direct parametric control

Guang Ren Duan
, Gang Xu

School of Astronautics

Harbin Institute of Technology

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

In this paper, a robust integrated translation and rotation tracking controller is proposed base on model reference tracking of quasi-linear system and direct parametric control approach for approaching non-cooperative target under the presence of parameter uncertainty. A tracking controller is provided in quasi-linear framework, which consists of the feedback stabilizing controller and the feed-froward compensator controller such that relative location between servicing spacecraft and target and relative attitude between chaser and the Earth can asymptotically tracking the given signal, the servicing spacecraft can observe the operating state or determine the fault point hovering on the non-cooperative target, further the integrative thruster layout is taking into account. A numerical simulation demonstrates the effect of the designed control strategy.

Original language	English
Title of host publication	Proceedings of the 35th Chinese Control Conference, CCC 2016
Editors	Jie Chen, Qianchuan Zhao, Jie Chen
Publisher	IEEE Computer Society
Pages	2940-2945
Number of pages	6
ISBN (Electronic)	9789881563910
DOIs	https://doi.org/10.1109/ChiCC.2016.7553810
State	Published - 26 Aug 2016
Event	35th Chinese Control Conference, CCC 2016 - Chengdu, China Duration: 27 Jul 2016 → 29 Jul 2016

Publication series

Name	Chinese Control Conference, CCC
Volume	2016-August
ISSN (Print)	1934-1768
ISSN (Electronic)	2161-2927

Conference

Conference	35th Chinese Control Conference, CCC 2016
Country/Territory	China
City	Chengdu
Period	27/07/16 → 29/07/16

Keywords

Direct Parametric Control
Integrated orbit and attitude control
Model reference tracking
Non-cooperative target
Thruster integration

Access to Document

10.1109/ChiCC.2016.7553810

Cite this

Duan, G. R., & Xu, G. (2016). Quasi-linear model reference tracking control of approaching non-cooperative target based on direct parametric control. In J. Chen, Q. Zhao, & J. Chen (Eds.), Proceedings of the 35th Chinese Control Conference, CCC 2016 (pp. 2940-2945). Article 7553810 (Chinese Control Conference, CCC; Vol. 2016-August). IEEE Computer Society. https://doi.org/10.1109/ChiCC.2016.7553810

@inproceedings{36fce61dd3f1444ab03a1728075f9e94,

title = "Quasi-linear model reference tracking control of approaching non-cooperative target based on direct parametric control",

abstract = "In this paper, a robust integrated translation and rotation tracking controller is proposed base on model reference tracking of quasi-linear system and direct parametric control approach for approaching non-cooperative target under the presence of parameter uncertainty. A tracking controller is provided in quasi-linear framework, which consists of the feedback stabilizing controller and the feed-froward compensator controller such that relative location between servicing spacecraft and target and relative attitude between chaser and the Earth can asymptotically tracking the given signal, the servicing spacecraft can observe the operating state or determine the fault point hovering on the non-cooperative target, further the integrative thruster layout is taking into account. A numerical simulation demonstrates the effect of the designed control strategy.",

keywords = "Direct Parametric Control, Integrated orbit and attitude control, Model reference tracking, Non-cooperative target, Thruster integration",

author = "Duan, \{Guang Ren\} and Gang Xu",

note = "Publisher Copyright: {\textcopyright} 2016 TCCT.; 35th Chinese Control Conference, CCC 2016 ; Conference date: 27-07-2016 Through 29-07-2016",

year = "2016",

month = aug,

day = "26",

doi = "10.1109/ChiCC.2016.7553810",

language = "英语",

series = "Chinese Control Conference, CCC",

publisher = "IEEE Computer Society",

pages = "2940--2945",

editor = "Jie Chen and Qianchuan Zhao and Jie Chen",

booktitle = "Proceedings of the 35th Chinese Control Conference, CCC 2016",

address = "美国",

}

Duan, GR & Xu, G 2016, Quasi-linear model reference tracking control of approaching non-cooperative target based on direct parametric control. in J Chen, Q Zhao & J Chen (eds), Proceedings of the 35th Chinese Control Conference, CCC 2016., 7553810, Chinese Control Conference, CCC, vol. 2016-August, IEEE Computer Society, pp. 2940-2945, 35th Chinese Control Conference, CCC 2016, Chengdu, China, 27/07/16. https://doi.org/10.1109/ChiCC.2016.7553810

Quasi-linear model reference tracking control of approaching non-cooperative target based on direct parametric control. / Duan, Guang Ren; Xu, Gang.
Proceedings of the 35th Chinese Control Conference, CCC 2016. ed. / Jie Chen; Qianchuan Zhao; Jie Chen. IEEE Computer Society, 2016. p. 2940-2945 7553810 (Chinese Control Conference, CCC; Vol. 2016-August).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Quasi-linear model reference tracking control of approaching non-cooperative target based on direct parametric control

AU - Duan, Guang Ren

AU - Xu, Gang

PY - 2016/8/26

Y1 - 2016/8/26

N2 - In this paper, a robust integrated translation and rotation tracking controller is proposed base on model reference tracking of quasi-linear system and direct parametric control approach for approaching non-cooperative target under the presence of parameter uncertainty. A tracking controller is provided in quasi-linear framework, which consists of the feedback stabilizing controller and the feed-froward compensator controller such that relative location between servicing spacecraft and target and relative attitude between chaser and the Earth can asymptotically tracking the given signal, the servicing spacecraft can observe the operating state or determine the fault point hovering on the non-cooperative target, further the integrative thruster layout is taking into account. A numerical simulation demonstrates the effect of the designed control strategy.

AB - In this paper, a robust integrated translation and rotation tracking controller is proposed base on model reference tracking of quasi-linear system and direct parametric control approach for approaching non-cooperative target under the presence of parameter uncertainty. A tracking controller is provided in quasi-linear framework, which consists of the feedback stabilizing controller and the feed-froward compensator controller such that relative location between servicing spacecraft and target and relative attitude between chaser and the Earth can asymptotically tracking the given signal, the servicing spacecraft can observe the operating state or determine the fault point hovering on the non-cooperative target, further the integrative thruster layout is taking into account. A numerical simulation demonstrates the effect of the designed control strategy.

KW - Direct Parametric Control

KW - Integrated orbit and attitude control

KW - Model reference tracking

KW - Non-cooperative target

KW - Thruster integration

UR - https://www.scopus.com/pages/publications/84987870710

U2 - 10.1109/ChiCC.2016.7553810

DO - 10.1109/ChiCC.2016.7553810

M3 - 会议稿件

AN - SCOPUS:84987870710

T3 - Chinese Control Conference, CCC

SP - 2940

EP - 2945

BT - Proceedings of the 35th Chinese Control Conference, CCC 2016

A2 - Chen, Jie

A2 - Zhao, Qianchuan

A2 - Chen, Jie

PB - IEEE Computer Society

T2 - 35th Chinese Control Conference, CCC 2016

Y2 - 27 July 2016 through 29 July 2016

ER -

Quasi-linear model reference tracking control of approaching non-cooperative target based on direct parametric control

Abstract

Publication series

Conference

Keywords

Access to Document

Other files and links

Fingerprint

Cite this