Boundary control design based on partial differential equation observer for vibration suppression and attitude control of flexible satellites with multi-section solar panels

Mohammad Mahdi Ataei, Hassan Salarieh, Hossein Nejat Pishkenari and Hadi Jalili, School of Mechanical Engineering, Sharif University of Technology, Iranian Space Research Institute

Journal of Vibration and Control

Published online on February 09, 2021

Abstract

Journal of Vibration and Control, Ahead of Print.
A novel partial differential equation observer is proposed to be used in boundary attitude and vibration control of flexible satellites. Solar panels’ vibrations and attitude dynamics form a coupled partial differential equation–ordinary differential ...