13.07.2015 Views

Formato PDF - mtc-m17:80 - Inpe

Formato PDF - mtc-m17:80 - Inpe

Formato PDF - mtc-m17:80 - Inpe

SHOW MORE
SHOW LESS
  • No tags were found...

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

ON DYNAMICS AND CONTROL OF SYSTEMS AND STRUCTURE IN SPACE,6., 2004. Liguria, Italy. Proceedings… Liguria, Italy:[s.n.],2004, p. 271-2<strong>80</strong>.ISBN 1 871315891.SOUZA, L. C G. design of satellite control system using optimal nonlineartheory. Mechanics Based Design of Structures and Machines, Taylor &Francis, v. 34, n. 4 p. 351-364, 2006.STEIN, G.; ATHANS, M. The LQG/LTR procedure for multivariable feedbackcontrol design. IEEE Transactions on Automatic Control, v. 32. n. 2, p. 105-104, Feb., 1987.STEYN, W. H., AND HASHIDA, Y. An attitude control system for a low-costearth observation satellite with orbit maintenance capability. In: AnnualAIAA/USU Conference on Small Satellites, 13., Logan, Utah, Proceedings…Logan: AIAA, 1999.TAHK, M. E SPEYER, J.L. Modelling of parameter variations and asymptoticlqg synthesis. IEEE Trans. Auto. Contr., v. AC-32, n.. 9, Sep., p. 793-<strong>80</strong>1,1987.VALDIVIA, R. H. V. Influência da flexibilidade no desempenho do sistemade controle de atitude de um satélite rígido/flexível. 2005-02-15. 105 p.(INPE-14209-TDI/1110). Dissertação de Mestrado - Instituto Nacional dePesquisas Espaciais, São José dos Campos. 2005. Disponível em:. Acesso em: 04 jul.2008.133

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!