Line-of-sight Tracking Control Scheme for Integrated Satellite with CMGs Vibration Isolation Platform

Han Wu; Lei Jin; Qinglei Hu; Yueyang Liu; Huanjie Wang; Fei Pan

doi:10.23919/CCC52363.2021.9550396

Line-of-sight Tracking Control Scheme for Integrated Satellite with CMGs Vibration Isolation Platform

Han Wu
, Lei Jin
, Qinglei Hu
, Yueyang Liu
, Huanjie Wang
, Fei Pan

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

3 Scopus citations

Abstract

This paper proposes an overall design scheme of Line-of-sight (LOS) tracking control for the integrated satellite system with vibration isolation platform (VIP) and control moment gyroscopes (CMGs). First, the three-axis attitude and motion trajectory are established for tracking the on-orbit dynamic target. To improve the accuracy and stability of target tracking, the VIP is applied to isolate CMGs micro vibration, and then controller parameters of integrated satellite system are synthetically designed based on the classical control theory. Subsequently, the effectiveness of the control scheme is verified by frequency and time domain simulation. The numerical examples show that the tracking accuracy can be increased by 80% and the stability can be improved by two orders of magnitude after adding VIP in the presence of the sample time of controller and the rotor static and dynamic imbalance.

Original language	English
Title of host publication	Proceedings of the 40th Chinese Control Conference, CCC 2021
Editors	Chen Peng, Jian Sun
Publisher	IEEE Computer Society
Pages	7707-7712
Number of pages	6
ISBN (Electronic)	9789881563804
DOIs	https://doi.org/10.23919/CCC52363.2021.9550396
State	Published - 26 Jul 2021
Event	40th Chinese Control Conference, CCC 2021 - Shanghai, China Duration: 26 Jul 2021 → 28 Jul 2021

Publication series

Name	Chinese Control Conference, CCC
Volume	2021-July
ISSN (Print)	1934-1768
ISSN (Electronic)	2161-2927

Conference

Conference	40th Chinese Control Conference, CCC 2021
Country/Territory	China
City	Shanghai
Period	26/07/21 → 28/07/21

Keywords

Classical control theory
Control moment gyroscopes
Line-of-sight tracking
Vibration isolation platform

Access to Document

10.23919/CCC52363.2021.9550396

Cite this

Wu, H., Jin, L., Hu, Q., Liu, Y., Wang, H., & Pan, F. (2021). Line-of-sight Tracking Control Scheme for Integrated Satellite with CMGs Vibration Isolation Platform. In C. Peng, & J. Sun (Eds.), Proceedings of the 40th Chinese Control Conference, CCC 2021 (pp. 7707-7712). (Chinese Control Conference, CCC; Vol. 2021-July). IEEE Computer Society. https://doi.org/10.23919/CCC52363.2021.9550396

@inproceedings{7ba31751d11641bd97feb5f625c4a256,

title = "Line-of-sight Tracking Control Scheme for Integrated Satellite with CMGs Vibration Isolation Platform",

abstract = "This paper proposes an overall design scheme of Line-of-sight (LOS) tracking control for the integrated satellite system with vibration isolation platform (VIP) and control moment gyroscopes (CMGs). First, the three-axis attitude and motion trajectory are established for tracking the on-orbit dynamic target. To improve the accuracy and stability of target tracking, the VIP is applied to isolate CMGs micro vibration, and then controller parameters of integrated satellite system are synthetically designed based on the classical control theory. Subsequently, the effectiveness of the control scheme is verified by frequency and time domain simulation. The numerical examples show that the tracking accuracy can be increased by 80\% and the stability can be improved by two orders of magnitude after adding VIP in the presence of the sample time of controller and the rotor static and dynamic imbalance.",

keywords = "Classical control theory, Control moment gyroscopes, Line-of-sight tracking, Vibration isolation platform",

author = "Han Wu and Lei Jin and Qinglei Hu and Yueyang Liu and Huanjie Wang and Fei Pan",

note = "Publisher Copyright: {\textcopyright} 2021 Technical Committee on Control Theory, Chinese Association of Automation.; 40th Chinese Control Conference, CCC 2021 ; Conference date: 26-07-2021 Through 28-07-2021",

year = "2021",

month = jul,

day = "26",

doi = "10.23919/CCC52363.2021.9550396",

language = "英语",

series = "Chinese Control Conference, CCC",

publisher = "IEEE Computer Society",

pages = "7707--7712",

editor = "Chen Peng and Jian Sun",

booktitle = "Proceedings of the 40th Chinese Control Conference, CCC 2021",

address = "美国",

}

Wu, H, Jin, L , Hu, Q, Liu, Y, Wang, H & Pan, F 2021, Line-of-sight Tracking Control Scheme for Integrated Satellite with CMGs Vibration Isolation Platform. in C Peng & J Sun (eds), Proceedings of the 40th Chinese Control Conference, CCC 2021. Chinese Control Conference, CCC, vol. 2021-July, IEEE Computer Society, pp. 7707-7712, 40th Chinese Control Conference, CCC 2021, Shanghai, China, 26/07/21. https://doi.org/10.23919/CCC52363.2021.9550396

Line-of-sight Tracking Control Scheme for Integrated Satellite with CMGs Vibration Isolation Platform. / Wu, Han; Jin, Lei ; Hu, Qinglei et al.
Proceedings of the 40th Chinese Control Conference, CCC 2021. ed. / Chen Peng; Jian Sun. IEEE Computer Society, 2021. p. 7707-7712 (Chinese Control Conference, CCC; Vol. 2021-July).

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

TY - GEN

T1 - Line-of-sight Tracking Control Scheme for Integrated Satellite with CMGs Vibration Isolation Platform

AU - Wu, Han

AU - Jin, Lei

AU - Hu, Qinglei

AU - Liu, Yueyang

AU - Wang, Huanjie

AU - Pan, Fei

PY - 2021/7/26

Y1 - 2021/7/26

N2 - This paper proposes an overall design scheme of Line-of-sight (LOS) tracking control for the integrated satellite system with vibration isolation platform (VIP) and control moment gyroscopes (CMGs). First, the three-axis attitude and motion trajectory are established for tracking the on-orbit dynamic target. To improve the accuracy and stability of target tracking, the VIP is applied to isolate CMGs micro vibration, and then controller parameters of integrated satellite system are synthetically designed based on the classical control theory. Subsequently, the effectiveness of the control scheme is verified by frequency and time domain simulation. The numerical examples show that the tracking accuracy can be increased by 80% and the stability can be improved by two orders of magnitude after adding VIP in the presence of the sample time of controller and the rotor static and dynamic imbalance.

AB - This paper proposes an overall design scheme of Line-of-sight (LOS) tracking control for the integrated satellite system with vibration isolation platform (VIP) and control moment gyroscopes (CMGs). First, the three-axis attitude and motion trajectory are established for tracking the on-orbit dynamic target. To improve the accuracy and stability of target tracking, the VIP is applied to isolate CMGs micro vibration, and then controller parameters of integrated satellite system are synthetically designed based on the classical control theory. Subsequently, the effectiveness of the control scheme is verified by frequency and time domain simulation. The numerical examples show that the tracking accuracy can be increased by 80% and the stability can be improved by two orders of magnitude after adding VIP in the presence of the sample time of controller and the rotor static and dynamic imbalance.

KW - Classical control theory

KW - Control moment gyroscopes

KW - Line-of-sight tracking

KW - Vibration isolation platform

UR - https://www.scopus.com/pages/publications/85117346123

U2 - 10.23919/CCC52363.2021.9550396

DO - 10.23919/CCC52363.2021.9550396

M3 - 会议稿件

AN - SCOPUS:85117346123

T3 - Chinese Control Conference, CCC

SP - 7707

EP - 7712

BT - Proceedings of the 40th Chinese Control Conference, CCC 2021

A2 - Peng, Chen

A2 - Sun, Jian

PB - IEEE Computer Society

T2 - 40th Chinese Control Conference, CCC 2021

Y2 - 26 July 2021 through 28 July 2021

ER -

Line-of-sight Tracking Control Scheme for Integrated Satellite with CMGs Vibration Isolation Platform

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