Control-oriented modelization of a satellite with large flexible appendages and use of worst-case analysis to verify robustness to model uncertainties of attitude control-Reference-Cited by-同舟云学术

Control-oriented modelization of a satellite with large flexible appendages and use of worst-case analysis to verify robustness to model uncertainties of attitude control

Published:2012-12 Issue:1 Volume:81 Page:214-226
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Gasbarri Paolo,Monti Riccardo,Campolo Giovanni,Toglia Chiara

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference12 articles.

1. P.M. Bainum, A.S.S.R. Reddy, R. Krishna, C.M. Diarra, V.K. Kumar, The Dynamics and Control of Large Flexible Space Structures—V, Nasa Report NSG-1414, Suppl. 4, 1982.

2. Dynamics and control of large space structures;Nurre;J. Guidance,1984

3. Constrained and unconstrained modes: some modeling aspects of flexible spacecraft;Hablani;AIAA J. Guidance Control,1980

4. Dynamics of multibody systems in space environments: Lagrangian vs. Eulerian approach;Santini;Acta Astronaut.,2004

5. Stability of flexible spacecraft;Santini;Acta Astronaut.,1976

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