Paper Info
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 relatively 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.
Year
DOI
Venue
2004
10.1109/ROBOT.2004.1307446
ICRA
Keywords
Field
DocType
flexible spacecraft,space vehicles,flexible appendages,aerospace control,rigid body motion,control system synthesis,time optimal control,component synthesis vibration suppression,vibration control,constant amplitude reaction jet thruster,time-fuel optimal control,optimal control
Vibration control,Optimal control,Active vibration control,Control theory,Rigid body,Robustness (computer science),Control engineering,Input shaping,Engineering,Vibration,Spacecraft
Conference
Volume
ISSN
ISBN
3
1050-4729
0-7803-8232-3
Citations 
PageRank 
References 
0
0.34
1
Authors
2
Name
Order
Citations
PageRank
Jinjun Shan181.15
Dong Sun296687.31