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

296 BIBLIOGRAPHIE[106] Losser, Y. Ajustement de lois de commande et application en aéronautique. PhD thesis, ÉcoleNationale Supérieure de l’Aéronautique et de l’Espace, Toulouse, France, March 24 2006.[107] Luenberger, D. G. An introduction to observers. IEEE Transactions on Automatic ControlAC-16, 6 (December 1971), 596–602.[108] Lurie, B. J. Multi-mode synchronized control for formation flying interferometer. In AIAAGuidance, Navigation, and Control Conference and Exhibit (Austin, TX, August 11-14 2003).[109] Magni, J.-F. Computation of the kernel of linear fractional representations. In IEEE Conferenceon Control Applications (Istanbul, Turkey, June 23-25 2003).[110] Magni, J.-F. Linear fractional representation toolbox. modelling, order reduction, gain scheduling.Tech. Rep. TR 6/08162, ONERA, Toulouse, France, July 2004.[111] Magni, J.-F. User manual of the linear fractional representation toolbox version 2.0. Tech.Rep. TR 5/10403.01 F DCSD, ONERA, 2006.[112] Magni, J.-F., Bennani, S., and Terlouw, J., Eds. Robust Flight Control : A Design Challenge.Springer, 1997.[113] Magni, J.-F., and Champetier, C. Lecture notes analyse et synthèse de lois de commandemodales. Supaéro, Toulouse, France, 1990.[114] Magni, J.-F., Knauf, A., and Döll, C. Practical implementation of LFT-scheduled feedbackgains. In 6th Asian Control Conference (Bali, Indonesia, July 18-21 2006).[115] Mailhé, L. M., and Guzmán, J. J. Initialization and resizing of formation flying using globaland local optimization methods. In 2004 IEEE Aerospace Conference (Big Sky, MT, March 6-132004), pp. 547–556.[116] Manceaux-Cumer, C. Techniques de commande robuste : approche par multiplicateurs etapproche stochastique. PhD thesis, École Nationale Supérieure de l’Aéronautique et de l’Espace,Toulouse, France, December 1998.[117] Manceaux-Cumer, C., and Chrétien, J.-P. Minimal LFT form of a spacecraft built upfrom two bodies. In AIAA Guidance, Navigation, and Control Conference and Exhibit (Montreal,Canada, August 6-9 2001).[118] Mandutianu, S., Hadaegh, F., and Elliot, P. Multi-agent system for formation flyingmissions. In 2001 IEEE Aerospace Conference (Big Sky, MT, March 10-17 2001), pp. 2793–2802.[119] Mannchen, T. Helicopter Vibration Reduction Using Robust Control. PhD thesis, Institut fürFlugmechanik und Flugregelung, Universität Stuttgart, Stuttgart, Germany, January 10 2003.[120] Marchal, C. The Three-Body Problem. Elsevier, Amsterdam, The Netherlands, 1990.[121] McQuade, F., Ward, R., and McInnes, C. R. The autonomous configuration of satelliteformation using a generic potential function. In 5th International Symposium on SpaceflightDynamics (Biarritz, France, June 26-30 2000).[122] Melton, R. G. Comparison of relative-motion models for elliptical orbits. In 3rd InternationalWorkshop on Satellite Constellations and Formation Flying (Pisa, Italy, 2003).Commande boucle fermée multivariable pour le vol en formation de vaisseaux spatiaux