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

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298 BIBLIOGRAPHIE[138] Philippe, C. ESA perspectives on advances control technology for comp<strong>le</strong>x space systems.Keynote <strong>le</strong>cture. IEEE Confer<strong>en</strong>ce on Control Applications. Munich, Germany, October 4-62006.[139] Piper, G. E., Watkins, J. M., and Leitner, J. A. On the impact of cross-link delayson spacecraft formation control. In AIAA Guidance, Navigation, and Control Confer<strong>en</strong>ce andExhibit (Austin, TX, August 11-14 2003).[140] Pirson, L., Charbonnel, C., Udrea, B., R<strong>en</strong>nie, M., McGuinness, P., and Palomo, P.Darwin precursor demonstration mission : The ICC2 study, from GNC design to real-time testb<strong>en</strong>ch validation. In 6th International ESA Confer<strong>en</strong>ce on Guidance, Navigation and ControlSystems (Loutraki, Greece, October 17-20, 2005).[141] Plo<strong>en</strong>, S. R., Hadaegh, F. Y., and Scharf, D. P. Rigid body equations of motion formodeling and control of spacecraft formations - part 1 : Absolute equations of motion. In 2004American Control Confer<strong>en</strong>ce (Boston, MA, USA, June 30-July 2 2004).[142] Plo<strong>en</strong>, S. R., Quadrelli, M. B., Scharf, D. P., and Hadaegh, F. Y. Dynamics ofdrag-free formations for earth imaging applications. In AIAA/AAS Astrodynamics SpecialistConfer<strong>en</strong>ce and Exhibit (Keystone, CO, USA, August 21-24 2006).[143] Pluym, J. P., and Damar<strong>en</strong>, C. J. Second order relative motion model for spacecraft underJ 2 perturbations. In AIAA/AAS Astrodynamics Specialist Confer<strong>en</strong>ce and Exhibit (Keystone,CO, USA, August 21-24 2006).[144] Purcell, G., Kuang, D., Licht<strong>en</strong>, S., Wu, S.-C., and Young, L. Autonomous formationflyer (aff) s<strong>en</strong>sor technology developm<strong>en</strong>t. Tech. Rep. TMO PR 42-134, Jet PropulsionLaboratory, California Institute of Technology, April-June 1998.[145] Richards, A., How, J., Schouw<strong>en</strong>aars, T., and Feron, E. Plume avoidance maneuverplanning using mixed integer linear programming. In AIAA Guidance, Navigation, and ControlConfer<strong>en</strong>ce and Exhibit (Montreal, Canada, August 6-9 2001).[146] Robertson, A., Inalhan, G., and How, J. P. Spacecraft formation flying control designfor the Orion mission. In AIAA Guidance, Navigation, and Control Confer<strong>en</strong>ce and Exhibit(Portland, OR, August 1999).[147] Robertson, A. D. Control System Design for Spacecraft Formation Flying : Theory andExperim<strong>en</strong>t. PhD thesis, Stanford University, Departm<strong>en</strong>t of Aeronautics and Astronautics,Stanford, CA, June 2001.[148] Romanelli, C. C., Natarajan, A., Schaub, H., Parker, G. G., and King, L. B. Coulombspacecraft <strong>vol</strong>tage study due to differ<strong>en</strong>tial orbital perturbation. In 2006 AAS/AIAA SpaceFlight Mechanics Meeting (Tampa, FL, January 22-26 2006).[149] Ross, I. M. Linearized dynamic equations for spacecraft subject to J 2 perturbations. Journalof Guidance, Control, and Dynamics 26, 4 (2003), 657–659.[150] Rugh, W. J. Linear System Theory. Pr<strong>en</strong>tice Hall, 1996.[151] Safonov, M. G., Goh, K. C., and Ly, J. H. Control system synthesis via bilinear matrixinequalities. In American Control Confer<strong>en</strong>ce (Baltimore, Maryland, June 1994), pp. 45–49.<strong>Commande</strong> <strong>bouc<strong>le</strong></strong> <strong>fermée</strong> <strong>multivariab<strong>le</strong></strong> <strong>pour</strong> <strong>le</strong> <strong>vol</strong> <strong>en</strong> formation de vaisseaux spatiaux

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