Boundary control design for vibration suppression and attitude control of flexible satellites with multi-section appendages

Author:

Ataei Mohammad MahdiORCID,Salarieh HassanORCID,Pishkenari Hossein NejatORCID,Jalili Hadi

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference31 articles.

1. Handbook of Satellite Applications;Pelton,2017

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3. Dynamic modeling for a flexible spacecraft with solar arrays composed of honeycomb panels and its proportional–derivative control with input shaper;Liu;ASME J. Dyn. Syst. Measu. Contr.,2016

4. Effects of uncertainties and flexible dynamic contributions on the control of a spacecraft full-coupled model;Gasbarri;Acta Astronaut.,2014

5. Thermally induced dynamics of satellite solar panels;Johnston;J. Spacecraft Rockets,2000

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