12.07.2015 Views

Commande boucle fermée multivariable pour le vol en ... - ISAE

Commande boucle fermée multivariable pour le vol en ... - ISAE

Commande boucle fermée multivariable pour le vol en ... - ISAE

SHOW MORE
SHOW LESS

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

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

Bibliographie[1] Absil, O. Sci<strong>en</strong>ce with Pegase. In 2nd TPF/Darwin Int. Confer<strong>en</strong>ce (San Diego, CA, July26-29 2004).[2] Alazard, D., and Apkarian, P. Exact observer-based structures for arbitrary comp<strong>en</strong>sators.International Journal on Robust and Nonlinear Control 9 (1999), 101–118.[3] Alazard, D., Cumer, C., Apkarian, P., Gauvrit, M., and Ferrères, G. Robustesse et<strong>Commande</strong> Optima<strong>le</strong>. Cépaduès Editions, 1999.[4] Alfri<strong>en</strong>d, K. T., and Schaub, H. Dynamics and control of spacecraft formations : Chal<strong>le</strong>ngesand some solutions. In Richard H. Battin Symposium (March 20-21 2000).[5] Alfri<strong>en</strong>d, K. T., and Schaub, H. Hybrid cartesian and orbit e<strong>le</strong>m<strong>en</strong>t feedback law forformation flying spacecraft. In AIAA Astrodynamics Specialist Confer<strong>en</strong>ce (D<strong>en</strong>ver, CO, August14-17 2000).[6] Alfri<strong>en</strong>d, K. T., Schaub, H., and Gim, D.-W. Gravitational perturbations, nonlinearityand circular orbit assumption effects on formation flying control strategies. In AAS RockyMountain Guidance & Control Confer<strong>en</strong>ce (Breck<strong>en</strong>ridge, CO, February 3-7 2000).[7] Alfri<strong>en</strong>d, K. T., and Yan, H. An orbital e<strong>le</strong>m<strong>en</strong>ts approach to the nonlinear formation flyingprob<strong>le</strong>m. In International Formation Flying Symposium (Toulouse, France, October 29-31 2002).[8] Alfri<strong>en</strong>d, K. T., and Yan, H. Evaluation and comparison of relative motion theories. Journalof Guidance, Control, and Dynamics 28, 2 (March-April 2005), 254–261.[9] Alonso, R., Crassidis, J. L., and Junkins, J. L. Vision-based relative navigation forformation flying of spacecraft. In AIAA Guidance, Navigation, and Control Confer<strong>en</strong>ce andExhibit (D<strong>en</strong>ver, Colorado, August 14-17 2000).[10] Alonso, R., Du, J.-Y., Hughes, D., Junkins, J. L., and Crassidis, J. L. Relative navigationfor formation flying of spacecraft. In Flight Mechanics Symposium (Gre<strong>en</strong>belt, Maryland,June 19-21 2001), NASA-Goddard Space Flight C<strong>en</strong>ter, pp. 115–129.[11] Aung, M., Ahmed, A., Wette, M., Scharf, D., Ti<strong>en</strong>, J., Purcell, G., Regehr, M.,and Landin, B. An overview of formation flying technology developm<strong>en</strong>t for the TerrestrialPlanet Finder mission. In 2004 IEEE Aerospace Confer<strong>en</strong>ce (Big Sky, MT, March 6-13 2004),pp. 2667–2679.[12] Balmino, G. Champ de pesanteur terrestre et géoïde. Principes, progrès et connaissance actuel<strong>le</strong>.http://bgi.cnes.fr:8110/tutorial/t2/tutorial2.html. [En ligne ; Page disponib<strong>le</strong><strong>le</strong> 29-juin-2006].289

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

Saved successfully!

Ooh no, something went wrong!