Attitude and vibration control of a satellite containing flexible solar arrays by using reaction wheels, and piezoelectric transducers as sensors and actuators-Reference-Cited by-同舟云学术

Attitude and vibration control of a satellite containing flexible solar arrays by using reaction wheels, and piezoelectric transducers as sensors and actuators

Published:2017-10 Issue: Volume:139 Page:357-366
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

da Fonseca Ijar M.,Rade Domingos A.,Goes Luiz C.S.,de Paula Sales Thiago

Publisher

Elsevier BV

Subject

Aerospace Engineering

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4. Cheng, G. Ianculescu, J. Ly, and M. Kim, “Control-structure interaction study for the space station solar dynamic power module,” in Proc. 30th IEEE Conf: Decis. Contz, Brighton, England, Dec. 1991, pp. 2219–2223.

5. Role of control-structure interaction in protective design;Dyke;ASCE J. Eng. Mech.,1995

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