Fast maneuver output feedback control for flexible spacecraft

Qiang Tang; Yan Wang; Xing Lin Chen

Fast maneuver output feedback control for flexible spacecraft

Qiang Tang^*
, Yan Wang
, Xing Lin Chen

^*Corresponding author for this work

School of Astronautics, Harbin Institute of Technology

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

Abstract

The output feedback control problem for flexible spacecraft fast maneuver was investigated. A more general passivity-based control law was proposed to meet the requirements of rapidity and vibration suppression. Then the Lyapunov method was used to analysis and proves asymptotic stability of the closed loop system. Simulation results of earth observation satellite during large angle rapid maneuvering show the effectiveness of the proposed control schemes.

Original language	English
Pages (from-to)	309-313
Number of pages	5
Journal	Zhongnan Daxue Xuebao (Ziran Kexue Ban)/Journal of Central South University (Science and Technology)
Volume	42
Issue number	SUPPL. 1
State	Published - Sep 2011
Externally published	Yes

Keywords

Fast maneuver
Flexible spacecraft
Output feedback
Passivity

Cite this

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title = "Fast maneuver output feedback control for flexible spacecraft",

abstract = "The output feedback control problem for flexible spacecraft fast maneuver was investigated. A more general passivity-based control law was proposed to meet the requirements of rapidity and vibration suppression. Then the Lyapunov method was used to analysis and proves asymptotic stability of the closed loop system. Simulation results of earth observation satellite during large angle rapid maneuvering show the effectiveness of the proposed control schemes.",

keywords = "Fast maneuver, Flexible spacecraft, Output feedback, Passivity",

author = "Qiang Tang and Yan Wang and Chen, \{Xing Lin\}",

year = "2011",

month = sep,

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volume = "42",

pages = "309--313",

journal = "Zhongnan Daxue Xuebao (Ziran Kexue Ban)/Journal of Central South University (Science and Technology)",

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publisher = "Central South University",

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TY - JOUR

T1 - Fast maneuver output feedback control for flexible spacecraft

AU - Tang, Qiang

AU - Wang, Yan

AU - Chen, Xing Lin

PY - 2011/9

Y1 - 2011/9

N2 - The output feedback control problem for flexible spacecraft fast maneuver was investigated. A more general passivity-based control law was proposed to meet the requirements of rapidity and vibration suppression. Then the Lyapunov method was used to analysis and proves asymptotic stability of the closed loop system. Simulation results of earth observation satellite during large angle rapid maneuvering show the effectiveness of the proposed control schemes.

AB - The output feedback control problem for flexible spacecraft fast maneuver was investigated. A more general passivity-based control law was proposed to meet the requirements of rapidity and vibration suppression. Then the Lyapunov method was used to analysis and proves asymptotic stability of the closed loop system. Simulation results of earth observation satellite during large angle rapid maneuvering show the effectiveness of the proposed control schemes.

KW - Fast maneuver

KW - Flexible spacecraft

KW - Output feedback

KW - Passivity

UR - https://www.scopus.com/pages/publications/82055193992

M3 - 文章

AN - SCOPUS:82055193992

SN - 1672-7207

VL - 42

SP - 309

EP - 313

JO - Zhongnan Daxue Xuebao (Ziran Kexue Ban)/Journal of Central South University (Science and Technology)

JF - Zhongnan Daxue Xuebao (Ziran Kexue Ban)/Journal of Central South University (Science and Technology)

IS - SUPPL. 1

ER -

Fast maneuver output feedback control for flexible spacecraft

Abstract

Keywords

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