Stabilizing the attitude of a flexible spacecraft with fast convergence

Shihong Ding; Wei Xing Zheng

doi:10.1109/WCICA.2012.6358147

Stabilizing the attitude of a flexible spacecraft with fast convergence

Research output: Chapter in Book / Conference Paper › Conference Paper › peer-review

Abstract

![CDATA[To achieve the high accuracy attitude stabilization, by utilizing finite-time control technique, a non-smooth attitude stabilizing control strategy for flexible spacecrafts is investigated in this paper. Based on a backstepping-like control scheme, the non-smooth attitude controller can be constructed step by step. The rigorous mathematical stability analysis of the overall closed-loop system is made by means of the cascaded systems theory. Simulation results show that not only can the attitude be stabilized precisely, but also the elastic vibration of flexible appendages can be suppressed effectively.]]

Original language	English
Title of host publication	Proceedings of the 10th World Congress on Intelligent Control and Automation, July 6-8, 2012, Beijing, China
Publisher	IEEE
Pages	1676-1681
Number of pages	6
ISBN (Print)	9781467313988
DOIs	https://doi.org/10.1109/WCICA.2012.6358147
Publication status	Published - 2012
Event	World Congress on Intelligent Control and Automation - Duration: 6 Jul 2012 → …

Conference

Conference	World Congress on Intelligent Control and Automation
Period	6/07/12 → …

Keywords

attitude control
attitude stabilization
finite-time control

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10.1109/WCICA.2012.6358147

Cite this

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title = "Stabilizing the attitude of a flexible spacecraft with fast convergence",

abstract = "![CDATA[To achieve the high accuracy attitude stabilization, by utilizing finite-time control technique, a non-smooth attitude stabilizing control strategy for flexible spacecrafts is investigated in this paper. Based on a backstepping-like control scheme, the non-smooth attitude controller can be constructed step by step. The rigorous mathematical stability analysis of the overall closed-loop system is made by means of the cascaded systems theory. Simulation results show that not only can the attitude be stabilized precisely, but also the elastic vibration of flexible appendages can be suppressed effectively.]]",

keywords = "attitude control, attitude stabilization, finite-time control",

author = "Shihong Ding and Zheng, {Wei Xing}",

year = "2012",

doi = "10.1109/WCICA.2012.6358147",

language = "English",

isbn = "9781467313988",

pages = "1676--1681",

booktitle = "Proceedings of the 10th World Congress on Intelligent Control and Automation, July 6-8, 2012, Beijing, China",

publisher = "IEEE",

note = "World Congress on Intelligent Control and Automation ; Conference date: 06-07-2012",

}

TY - GEN

T1 - Stabilizing the attitude of a flexible spacecraft with fast convergence

AU - Ding, Shihong

AU - Zheng, Wei Xing

PY - 2012

Y1 - 2012

N2 - ![CDATA[To achieve the high accuracy attitude stabilization, by utilizing finite-time control technique, a non-smooth attitude stabilizing control strategy for flexible spacecrafts is investigated in this paper. Based on a backstepping-like control scheme, the non-smooth attitude controller can be constructed step by step. The rigorous mathematical stability analysis of the overall closed-loop system is made by means of the cascaded systems theory. Simulation results show that not only can the attitude be stabilized precisely, but also the elastic vibration of flexible appendages can be suppressed effectively.]]

AB - ![CDATA[To achieve the high accuracy attitude stabilization, by utilizing finite-time control technique, a non-smooth attitude stabilizing control strategy for flexible spacecrafts is investigated in this paper. Based on a backstepping-like control scheme, the non-smooth attitude controller can be constructed step by step. The rigorous mathematical stability analysis of the overall closed-loop system is made by means of the cascaded systems theory. Simulation results show that not only can the attitude be stabilized precisely, but also the elastic vibration of flexible appendages can be suppressed effectively.]]

KW - attitude control

KW - attitude stabilization

KW - finite-time control

UR - http://handle.uws.edu.au:8081/1959.7/524083

UR - http://2012.wcica.info/

U2 - 10.1109/WCICA.2012.6358147

DO - 10.1109/WCICA.2012.6358147

M3 - Conference Paper

SN - 9781467313988

SP - 1676

EP - 1681

BT - Proceedings of the 10th World Congress on Intelligent Control and Automation, July 6-8, 2012, Beijing, China

PB - IEEE

T2 - World Congress on Intelligent Control and Automation

Y2 - 6 July 2012

ER -

Stabilizing the attitude of a flexible spacecraft with fast convergence

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Keywords

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