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

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Liste des publications[1] Gaulocher, S. Modeling the coup<strong>le</strong>d translational and rotational relative dynamics for formationflying control. In AIAA Guidance, Navigation, and Control Confer<strong>en</strong>ce and Exhibit (SanFranciso, CA, August 2005).[2] Gaulocher, S. Modélisation de la dynamique relative couplée <strong>en</strong> translation/rotation <strong>pour</strong> <strong>le</strong>contrô<strong>le</strong> du <strong>vol</strong> <strong>en</strong> formation. In 6ème Congrès des Doctorants de l’Éco<strong>le</strong> Doctora<strong>le</strong> Systèmes(Toulouse, France, May 19-20 2005).[3] Gaulocher, S., Chréti<strong>en</strong>, J.-P., and Pittet, C. Six-DOF formation flying modeling andcontrol with an application to space interferometry. In 6th International ESA Confer<strong>en</strong>ce onGuidance, Navigation and Control Systems (Loutraki, Greece, October 17-20, 2005).[4] Gaulocher, S., Chréti<strong>en</strong>, J.-P., and Pittet, C. Six-axis control design and control<strong>le</strong>r switchingfor spacecraft formation flying. In AIAA Guidance, Navigation, and Control Confer<strong>en</strong>ceand Exhibit (Keystone, CO, August 2006).[5] Gaulocher, S., Chréti<strong>en</strong>, J.-P., Pittet, C., Delpech, M., and Alazard, D. Closedloopcontrol of formation flying satellites : Time and parameter varying framework. In 2nd Int.Symposium on Formation Flying Missions & Technologies (Washington, DC, September 14-162004).[6] Gaulocher, S., Chréti<strong>en</strong>, J.-P., Pittet, C., and Alazard, D. Six-axis dec<strong>en</strong>tralizedcontrol design for spacecraft formation flying. In IEEE International Confer<strong>en</strong>ce on ControlApplications (Munich, Germany, October 4-6 2006).[7] Gaulocher, S., Cumer, C., Alazard, D., Humbert, M., and Cassein, G. Aircraft loadal<strong>le</strong>viation during manoeuvres using optimal control surfaces combinations. In 6th ONERA-DLRAerospace Symposium (Berlin, Germany, June 22-23 2004).[8] Gaulocher, S., Pittet, C., and Chréti<strong>en</strong>, J.-P. Modélisation de la dynamique relativecouplée <strong>en</strong> translation/rotation <strong>pour</strong> <strong>le</strong> contrô<strong>le</strong> du <strong>vol</strong> <strong>en</strong> formation de satellites. In JournéesDoctora<strong>le</strong>s et Nationa<strong>le</strong>s du GDR MACS (Lyon, France, September 5-7 2005).[9] Gaulocher, S., Roos, C., and Cumer, C. Aircraft load al<strong>le</strong>viation during maneuversusing optimal control surface combinations. Journal of Guidance, Control, and Dynamics 30, 2(March-April 2007).[10] Knauf, A., Gaulocher, S., and Feuersänger, A. P. Innovative control<strong>le</strong>r design forsystems with parameter variations. In Deutscher Luft- und Raumfahrtkongress (Braunschweig,Germany, November 6-9 2006).xxi

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