Robust component synthesis vibration suppression for maneuver of flexible spacecrafts

Jinjun Shan; Dong Sun

doi:10.1109/ROBOT.2004.1307446

Robust component synthesis vibration suppression for maneuver of flexible spacecrafts

Jinjun Shan, Dong Sun

Research output: Journal Publications and Reviews › RGC 22 - Publication in policy or professional journal

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Abstract

This paper presents a development of component synthesis vibration suppression (CSVS) method for control of spacecrafts with large flexible appendages. The proposed method eliminates unwanted flexible modes of vibrations while achieving the desired rigid body motion. Unlike traditional input shaping in which a numerical optimization is utilized, design for CSVS commands is based on analytic methodology and is relative easy to implement. The robustness to uncertainties of dynamic modeling parameters is analyzed. A case study is performed on a time-fuel optimal control strategy using constant amplitude reaction jet thrusters. Both simulation and experimental results validate the effectiveness of the CSVS approach.

Original language	English
Pages (from-to)	2556-2561
Journal	Proceedings - IEEE International Conference on Robotics and Automation
Volume	2004
Issue number	3
DOIs	https://doi.org/10.1109/ROBOT.2004.1307446
Publication status	Published - 2004
Event	Proceedings- 2004 IEEE International Conference on Robotics and Automation - New Orleans, LA, United States Duration: 26 Apr 2004 → 1 May 2004

Research Keywords

Component synthesis vibration suppression
Experimental study
Optimal control
Robustness

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title = "Robust component synthesis vibration suppression for maneuver of flexible spacecrafts",

abstract = "This paper presents a development of component synthesis vibration suppression (CSVS) method for control of spacecrafts with large flexible appendages. The proposed method eliminates unwanted flexible modes of vibrations while achieving the desired rigid body motion. Unlike traditional input shaping in which a numerical optimization is utilized, design for CSVS commands is based on analytic methodology and is relative easy to implement. The robustness to uncertainties of dynamic modeling parameters is analyzed. A case study is performed on a time-fuel optimal control strategy using constant amplitude reaction jet thrusters. Both simulation and experimental results validate the effectiveness of the CSVS approach.",

keywords = "Component synthesis vibration suppression, Experimental study, Optimal control, Robustness",

author = "Jinjun Shan and Dong Sun",

year = "2004",

doi = "10.1109/ROBOT.2004.1307446",

language = "English",

volume = "2004",

pages = "2556--2561",

journal = "Proceedings - IEEE International Conference on Robotics and Automation",

issn = "1050-4729",

publisher = "IEEE",

number = "3",

note = "Proceedings- 2004 IEEE International Conference on Robotics and Automation ; Conference date: 26-04-2004 Through 01-05-2004",

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TY - JOUR

T1 - Robust component synthesis vibration suppression for maneuver of flexible spacecrafts

AU - Shan, Jinjun

AU - Sun, Dong

PY - 2004

Y1 - 2004

N2 - This paper presents a development of component synthesis vibration suppression (CSVS) method for control of spacecrafts with large flexible appendages. The proposed method eliminates unwanted flexible modes of vibrations while achieving the desired rigid body motion. Unlike traditional input shaping in which a numerical optimization is utilized, design for CSVS commands is based on analytic methodology and is relative easy to implement. The robustness to uncertainties of dynamic modeling parameters is analyzed. A case study is performed on a time-fuel optimal control strategy using constant amplitude reaction jet thrusters. Both simulation and experimental results validate the effectiveness of the CSVS approach.

AB - This paper presents a development of component synthesis vibration suppression (CSVS) method for control of spacecrafts with large flexible appendages. The proposed method eliminates unwanted flexible modes of vibrations while achieving the desired rigid body motion. Unlike traditional input shaping in which a numerical optimization is utilized, design for CSVS commands is based on analytic methodology and is relative easy to implement. The robustness to uncertainties of dynamic modeling parameters is analyzed. A case study is performed on a time-fuel optimal control strategy using constant amplitude reaction jet thrusters. Both simulation and experimental results validate the effectiveness of the CSVS approach.

KW - Component synthesis vibration suppression

KW - Experimental study

KW - Optimal control

KW - Robustness

UR - http://www.scopus.com/inward/record.url?scp=3042664658&partnerID=8YFLogxK

UR - https://www.scopus.com/record/pubmetrics.uri?eid=2-s2.0-3042664658&origin=recordpage

U2 - 10.1109/ROBOT.2004.1307446

DO - 10.1109/ROBOT.2004.1307446

M3 - RGC 22 - Publication in policy or professional journal

SN - 1050-4729

VL - 2004

SP - 2556

EP - 2561

JO - Proceedings - IEEE International Conference on Robotics and Automation

JF - Proceedings - IEEE International Conference on Robotics and Automation

IS - 3

T2 - Proceedings- 2004 IEEE International Conference on Robotics and Automation

Y2 - 26 April 2004 through 1 May 2004

ER -

Robust component synthesis vibration suppression for maneuver of flexible spacecrafts

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Research Keywords

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