Vibration Control Design of Fuel Sloshing in a Spacecraft Using Virtual Actuator

This paper is dedicated to modeling of fuel sloshing dynamics and its effect on the stability and control of the space vehicle. Sloshing due to the liquid movement in the fuel tank of a space vehicle's propulsion system can be effective on the vehicle’s control and stability. Force and moment i...

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Bibliographic Details

Published in:	فصلنامه علوم و فناوری فضایی
Main Authors:	Abdolmajid khoshnood, Ali Aminzadeh, Peyman Nikpey
Format:	Article
Language:	Persian
Published:	Aerospace Research Institute 2022-03-01
Subjects:	fuel sloshing spacecraft mass-spring model virtual actuator lqr
Online Access:	https://jsst.ias.ir/article_132801_8feab2a335f4ae75fa168c7d52fc1bf1.pdf