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300 BIBLIOGRAPHIE[167] Stilwell, D. J., and Rugh, W. J. Interpolation of observer state feedback controllers forgain scheduling. IEEE Transactions on Automatic Control 44, 6 (June 1999), 1225–1229.[168] Swinkels, B. L. High-accuracy absolute distance metrology. PhD thesis, TU Delft, Delft, TheNetherlands, September 2006.[169] Tanygin, S., and Woodburn, J. Attitude covariance visualization. In AIAA/AAS AstrodynamicsSpecialist Conference and Exhibit (Monterey, CA, August 5-8 2002).[170] Théron, A., Jouhaud, F., and Chrétien, J.-P. Modélisation du mouvement orbital relatifentre deux satellites. Tech. Rep. NI 1/08282 DCSD, ONERA-DCSD, Toulouse, France, January2004.[171] Tillerson, M., and How, J. P. Formation flying control in eccentrc orbits. In AIAAGuidance, Navigation, and Control Conference and Exhibit (Montreal, Canada, August 6-92001).[172] Tillerson, M., and How, J. P. Advanced guidance algorithms for spacecraft formationkeeping.In American Control Conference (2002).[173] Tillerson, M., Inalhan, G., and How, J. P. Co-ordination and control of distributedspacecraft systems using convex optimization techniques. International Journal of Robust andNonlinear Control 12 (2002), 207–242.[174] Tillerson, M. J. Coordination and control of multiple spacecraft using convex optimizationtechniques. Master’s thesis, Massachusetts Institute of Technology, Cambridge, MA, June 2002.[175] Tschauner, J. Elliptic orbit rendezvous. AIAA Journal 5, 6 (1967), 1110–1113.[176] Turner, M. C., Aouf, N., Bates, D. G., Postlethwaite, I., and Boulet, B. Switchedcontrol of a vertical/short take-off land aircraft : an application of linear quadratic bumplesstransfer. Proceedings of The Institution of Mechanical Engineers Part I, Journal of Systems andControl Engineering 220 (2006), 157–170.[177] Vadali, S. R., Vaddi, S. S., and Alfriend, K. T. An intelligent control concept for formationflying satellite constellations. International Journal of Robust and Nonlinear Control 12,2-3 (2000), 97–115.[178] Vadali, S. R., Vaddi, S. S., Naik, K., and Alfriend, K. T. Control of satellite formations.In AIAA Guidance, Navigation, and Control Conference and Exhibit (Montreal, Canada, August6-9 2001).[179] Vaddi, S. S., Alfriend, K. T., Vadali, S. R., and Sengupta, P. Formation establishmentand reconfiguration using impulsive control. Journal of Guidance, Control, and Dynamics 28,2 (March-April 2005), 262–268.[180] Valentin Luangraj, S. Vers une approche non-linéaire de la commande d’attitude de satellitespar jets de gaz. PhD thesis, École Nationale Supérieure de l’Aéronautique et de l’Espace,Toulouse, France, December 16 2004.[181] VanDyke, M. C. Decentralized attitude control of a formation of spacecraft. In 2004 AIAARegion I-MA Student Conference (Blacksburg, VA, April 16-18 2004).Commande boucle fermée multivariable pour le vol en formation de vaisseaux spatiaux
BIBLIOGRAPHIE 301[182] Varga, A. New numerical software for model and controller reduction. Tech. rep., SLICOTWorking Note SLWN2002-5, 2002. http://elib.dlr.de/11855/01/varga_SLWN2002-5.pdf.[183] Vesely, F. J. Shortest distance between two ellipses or ellipsoids. http://homepage.univie.ac.at/franz.vesely/texte/hard_ellipse/hell/, July 2002. [En ligne ; Page disponible le29-juin-2006].[184] Wang, P. K. C., Hadaegh, F. Y., and Lau, K. Synchronized formation rotation andattitude control of multiple free-flying spacecraft. Journal of Guidance, Control, and Dynamics22, 1 (January-February 1999), 28–35.[185] Wie, B. Space Vehicle Dynamics and Control, 1 ed. AIAA Education Series. American Instituteof Aeronautics and Astronautics, Reston, VA, USA, 1998.[186] Wikipédia. Gravitation — Wikipédia, l’encyclopédie libre. http://fr.wikipedia.org/w/index.php?title=Gravitation&oldid=8010201, 2006. [En ligne ; Page disponible le 29-juin-2006].[187] Wikipédia. Harmonique sphérique — Wikipédia, l’encyclopédie libre. http://fr.wikipedia.org/w/index.php?title=Harmonique_sph%C3%A9rique&oldid=6902888, 2006. [En ligne ;Page disponible le 29-juin-2006].[188] Wikipédia. Lois de kepler — Wikipédia, l’encyclopédie libre. http://fr.wikipedia.org/w/index.php?title=Lois_de_Kepler&oldid=9582526, 2006. [En ligne ; Page disponible le 29-juin-2006].[189] Wikipédia. Soleil — Wikipédia, l’encyclopédie libre. http://fr.wikipedia.org/w/index.php?title=Soleil&oldid=8268548, 2006. [En ligne ; Page disponible le 29-juin-2006].[190] Wikipédia. Terre — Wikipédia, l’encyclopédie libre. http://fr.wikipedia.org/w/index.php?title=Terre&oldid=8191160, 2006. [En ligne ; Page disponible le 29-juin-2006].[191] Wikipédia. Unité astronomique — Wikipédia, l’encyclopédie libre. http://fr.wikipedia.org/w/index.php?title=Unit%C3%A9_astronomique&oldid=10221382, 2006. [En ligne ; Pagedisponible le 29-juin-2006].[192] Won, C.-H., and Ahn, H.-S. Nonlinear orbital dynamic equations and state-dependent riccatiequation control of formation flying satellites. Journal of the Astronautical Sciences 51, 4(October-December 2003).[193] Wong, H., and Kapila, V. Spacecraft formation flying near sun-earth L 2 lagrange point : Trajectorygeneration and adaptive output feedback control. In 2005 American Control Conference(Portland, OR, June 8-10 2005).[194] Wong, H., Kapila, V., and Sparks, A. Adaptive output feedback tracking control of multiplespacecraft. In American Control Conference (Arlington, VA, June 25-27 2001).[195] Wong, H., Pan, H., de Queiroz, M. S., and Kapila, V. Adaptive learning control forspacecraft formation flying. In 40th IEEE Conference on Decision and Control (Orlando, FL,December 2001).[196] Wong, H., Pan, H., and Kapila, V. Output feedback control for spacecraft formationflying with coupled translation and attitude dynamics. In 2005 American Control Conference(Portland, OR, USA, June 8-10 2005).Commande boucle fermée multivariable pour le vol en formation de vaisseaux spatiaux
Page 1:
THÈSEEn vue de l'obtention duDOCTO
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iRemerciementsÀ l’issue de la lo
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viTABLE DES MATIÈRESII Modèles po
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viiiTABLE DES MATIÈRES4.5.4 Probl
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xTABLE DES MATIÈRESE Non-existence
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xiiSIGLES ET ACRONYMESSigleExplicat
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xivTABLE DES FIGURES3.2 Orbite halo
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xviTABLE DES FIGURES5.9 Effet d’u
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Liste des tableaux1.1 Missions de v
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Liste des publications[1] Gaulocher
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Première partieIntroduction1
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4 1. LE VOL EN FORMATIONLe vol en f
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6 1. LE VOL EN FORMATIONLa Fig. 1.3
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8 1. LE VOL EN FORMATIONSoleil. Le
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10 1. LE VOL EN FORMATIONFigure 1.6
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12 1. LE VOL EN FORMATIONÀ l’int
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14 1. LE VOL EN FORMATIONque d’ha
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16 1. LE VOL EN FORMATIONLa Fig. 1.
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Deuxième partieModèles pour le vo
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22 2. DYNAMIQUE TRANSLATIONNELLE EN
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60 3. MODÈLE COUPLÉ EN TRANSLATIO
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100 3. MODÈLE COUPLÉ EN TRANSLATI
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Chapitre 4Méthodologie pour le pil
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4.1 Revue bibliographique 129Hussei
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4.2 Objectifs 131du système en bou
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4.3 Analyse de la dynamique 133d’
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4.3 Analyse de la dynamique 1352402
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4.4 Modèle linéaire fractionnaire
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4.5 Contrôle modal auto-séquencé
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4.6 Contrôle séquencé H 2 -optim
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Chapitre 5Méthodologie pour le pil
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5.1 Revue bibliographique 185Planet
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5.3 Modélisation de la mission Peg
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5.4 Synthèse d’un correcteur pou
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5.5 Commutation entre correcteurs 2
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Page 275 and 276: 5.5 Commutation entre correcteurs 2
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Page 305: 5.7 Bilan global 279complètement d
Page 309 and 310: Récapitulation et contributionsDan
Page 311: RÉCAPITULATION ET CONTRIBUTIONS 28
Page 314 and 315: 288 PERSPECTIVESde base pour le mod
Page 316 and 317: 290 BIBLIOGRAPHIE[13] Bamford, W. A
Page 318 and 319: 292 BIBLIOGRAPHIE[44] Dailey, R. L.
Page 320 and 321: 294 BIBLIOGRAPHIE[75] Hussein, I. I
Page 322 and 323: 296 BIBLIOGRAPHIE[106] Losser, Y. A
Page 324 and 325: 298 BIBLIOGRAPHIE[138] Philippe, C.
Page 328 and 329: 302 BIBLIOGRAPHIE[197] Yamamoto, T.
Page 331: Annexe AConstantes et unitésConsta
Page 334 and 335: 308 B. NOTATIONSLe carré d’une m
Page 336 and 337: 310 B. NOTATIONSLa dérivée tempor
Page 339 and 340: Annexe CNotions de base en cinémat
Page 341 and 342: C.1 Cinématique 315Figure C.1 - Un
Page 343 and 344: C.1 Cinématique 317Cette matrice e
Page 345 and 346: C.1 Cinématique 319Nous utiliseron
Page 347 and 348: C.1 Cinématique 321Il est possible
Page 349 and 350: C.2 Dynamique 323l’expression (C.
Page 351 and 352: C.2 Dynamique 325Figure C.5 - Corps
Page 353 and 354: C.2 Dynamique 327= m −→ •−
Page 355 and 356: Annexe DCalcul des gradients et hes
Page 357 and 358: D.2 Deuxième harmonique zonal (J 2
Page 359 and 360: Annexe ENon-existence d’une repr
Page 361 and 362: 335- Condition d’ordre trois (N =
Page 363 and 364: Annexe FTransformée de Fourier dis
Page 365 and 366: Annexe GThéorème de Floquet ettra
Page 367: 341Le logarithme naturel log z d’
Page 370 and 371: 344 H. LA SYNTHÈSE H 2Les dimensio
Page 372 and 373: 346 H. LA SYNTHÈSE H 2Tout d’abo
Page 375 and 376: Annexe IDistance entre un hyper-ell
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I.1 Premier algorithme 351longueurs
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I.2 Deuxième algorithme 353˜x (k)
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I.2 Deuxième algorithme 355Mainten
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Annexe JRéduction de correcteursL
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359Le critère pour la réduction d
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