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
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302 BIBLIOGRAPHIE[197] Yamamoto, T. Practical analytic solution of relative motion betwe<strong>en</strong> formation flying satelliteswith differ<strong>en</strong>t ballistic coeffici<strong>en</strong>ts in the near-circular refer<strong>en</strong>ce orbit. In 6th International ESAConfer<strong>en</strong>ce on Guidance, Navigation and Control Systems (Loutraki, Greece, October 17-202005).[198] Yamanaka, K. Simultaneous translation and rotation control law for formation flying satellites.In AIAA Guidance, Navigation, and Control Confer<strong>en</strong>ce and Exhibit (D<strong>en</strong>ver, CO, August 14-172000).[199] Yamanaka, K., and Ankers<strong>en</strong>, F. New state transition matrix for relative motion on anarbitrary elliptical orbit. Journal of Guidance, Control, and Dynamics 25, 1 (2002), 60–66.[200] Yan, Q., Kapila, V., and Sparks, A. G. Pulse-based periodic control for spacecraft formationflying. In 2000 American Control Confer<strong>en</strong>ce (Chicago, IL, June 2000).[201] Yan, Q., Yang, G., Kapila, V., and de Queiroz, M. S. Nonlinear dynamics and outputfeedback control of multip<strong>le</strong> spacecraft in elliptical orbits. In 2000 American Control Confer<strong>en</strong>ce(Chicago, IL, June 2000).[202] Yang, G., Yang, Q., Kapila, V., Palmer, D., and Vaidyanathan, R. Fuel optimalmaneuvers for multip<strong>le</strong> spacecraft formation reconfiguration using multi-ag<strong>en</strong>t optimization. In40th IEEE Confer<strong>en</strong>ce on Decision and Control (Orlando, FL, December 2001).[203] Yedavalli, R. K., and Sparks, A. Satellite formation keeping control design based onultimate bounded analysis of switched systems. In AIAA Guidance, Navigation, and ControlConfer<strong>en</strong>ce and Exhibit (Montreal, Canada, August 6-9 2001).[204] Yedavalli, R. K., and Sparks, A. G. Satellite formation flying control design based onhybrid control system stability analysis. In 2000 American Control Confer<strong>en</strong>ce (Chicago, IL,June 2000).[205] Zarrouati, O. Trajectoires spatia<strong>le</strong>s.Cépaduès-Éditions, Toulouse, France, 1987.[206] Zhang, F., and Krishnaprasad, P. S. Formation dynamics under a class of control laws.Tech. rep., Institute of for Systems Research, University of Maryland at Col<strong>le</strong>ge Park, Col<strong>le</strong>gePark, MD, 2002.[207] Zhang, H., and Sun, L. Spacecraft formation-flying in ecc<strong>en</strong>tric orbits. In AIAA Guidance,Navigation, and Control Confer<strong>en</strong>ce and Exhibit (Austin, TX, August 11-14 2003).[208] Zuo, L., and Nayfeh, S. A. Structured H 2 optimization of vehic<strong>le</strong> susp<strong>en</strong>sions based onmulti-wheel models. Vehic<strong>le</strong> System Dynamics 40, 5 (2003), 351–371.<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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