Boundary control design based on partial differential equation observer for vibration suppression and attitude control of flexible satellites with multi-section solar panels
Author:
Affiliation:
1. School of Mechanical Engineering, Sharif University of Technology, Iran
2. Iranian Space Research Institute, Iran
Abstract
Funder
Iranian Space Research Center
Publisher
SAGE Publications
Subject
Mechanical Engineering,Mechanics of Materials,Aerospace Engineering,Automotive Engineering,General Materials Science
Link
http://journals.sagepub.com/doi/pdf/10.1177/1077546321990158
Reference28 articles.
1. Vibration suppression of smart nonlinear flexible appendages of a rotating satellite by using hybrid adaptive sliding mode/Lyapunov control
2. A hybrid control scheme for attitude and vibration suppression of a flexible spacecraft using energy-based actuators switching mechanism
3. Boundary vibration control for a two-link rigid–flexible manipulator with quantized input
4. Flexible satellite attitude maneuver via constrained torque distribution and active vibration suppression
5. Boundary control of a rotating shear beam with observer feedback
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