Vibration Suppression of a Maneuvering Flexible Spacecraft with Actuator Dynamic

This paper presents a study concerning active vibration control of a smart, flexible spacecraft during attitude maneuver using thrusters/ a reaction wheel and piezoelectric patches. The large-angle maneuver and residual vibration of the spacecraft are controlled utilizing an extended Lyapunov-based...

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Bibliographic Details

Published in:	فناوری در مهندسی هوافضا
Main Authors:	Milad Azimi, Samad Moradi
Format:	Article
Language:	Persian
Published:	Aerospace Research Institute (ARI) 2021-05-01
Subjects:	thrusters vibration control flexible spacecraft lyapunov controller piezoelectric patches
Online Access:	https://jtae.ari.ac.ir/article_129873_4e42579b75216fecf458e62e1564ae2c.pdf