Passive vibration control of flexible spacecraft using shunted piezoelectric transducers

Author:

Sales T.P.,Rade D.A.,de Souza L.C.G.

Funder

Brazilian Research Agency CNPq

CNPq

National Institute of Sciences and Technology of Smart Structures in Engineering (INCT-EIE)

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference30 articles.

1. Vibration suppression and adaptive-robust control of a smart flexible satellite with three axes maneuvering;Azadi;Acta Astronautica,2011

2. Flexible spacecraft attitude maneuver by application of sliding mode control;Bang;Acta Astronautica,2005

3. Predictive control for the attitude maneuver of a flexible spacecraft;Bang;Aerospace Science and Technology,2004

4. Experimental design of a flexible satellite attitude control system using the H-infinity method;Castro;Advances in the Astronautical Sciences,2010

5. Fundamentals of Structural Dynamics;Craig,2011

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