Design of a controller for a rigid-flexible satellite using the H-infinity method considering the parametric uncertainty-Reference-Cited by-同舟云学术

Design of a controller for a rigid-flexible satellite using the H-infinity method considering the parametric uncertainty

Published:2019-02 Issue: Volume:116 Page:641-650
ISSN:0888-3270
Container-title:Mechanical Systems and Signal Processing
language:en
Short-container-title:Mechanical Systems and Signal Processing

Author:

Souza A.G.,Souza L.C.G.

Funder

CAPES

INPE

DMC

Publisher

Elsevier BV

Subject

Computer Science Applications,Mechanical Engineering,Aerospace Engineering,Civil and Structural Engineering,Signal Processing,Control and Systems Engineering

Reference12 articles.

1. Spacecraft Dynamics and Control: A Practical Engineering Approach;Sidi,1997

2. Flexibility issues in discrete on-off actuated spacecraft: numerical and experimental tests;Gasbarri;Acta Astronaut.,2014

3. Introduction to Dynamics and Control of Flexible Structures;Junkins,1993

4. H infinity controller design to a rigid-flexible satellite with two vibration modes;Souza;J. Phys.: Conf. Ser.,2015

5. Satellite attitude control system design considering the fuel slosh dynamics;Souza;Shock Vib.,2014

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