{"id":104,"date":"2024-09-26T10:21:18","date_gmt":"2024-09-26T08:21:18","guid":{"rendered":"https:\/\/dev.mon-studio-web.com\/dycsyt\/?page_id=104"},"modified":"2024-10-07T11:02:30","modified_gmt":"2024-10-07T09:02:30","slug":"ressources","status":"publish","type":"page","link":"https:\/\/dev.mon-studio-web.com\/dycsyt\/ressources\/","title":{"rendered":"Ressources"},"content":{"rendered":"

[et_pb_section fb_built=\u00a0\u00bb1″ _builder_version=\u00a0\u00bb4.26.1″ _module_preset=\u00a0\u00bbdefault\u00a0\u00bb background_color=\u00a0\u00bb#0c0c0c\u00a0\u00bb custom_margin=\u00a0\u00bb40px||150px||false|false\u00a0\u00bb custom_margin_tablet=\u00a0\u00bb85px||150px||false|false\u00a0\u00bb custom_margin_phone=\u00a0\u00bb60px||100px||false|false\u00a0\u00bb custom_margin_last_edited=\u00a0\u00bbon|tablet\u00a0\u00bb custom_padding=\u00a0\u00bb120px||0px||false|false\u00a0\u00bb hover_enabled=\u00a0\u00bb0″ locked=\u00a0\u00bboff\u00a0\u00bb global_colors_info=\u00a0\u00bb{}\u00a0\u00bb sticky_enabled=\u00a0\u00bb0″][et_pb_row _builder_version=\u00a0\u00bb4.26.1″ _module_preset=\u00a0\u00bbdefault\u00a0\u00bb custom_margin=\u00a0\u00bb-35px|auto|1px|auto|false|false\u00a0\u00bb custom_padding=\u00a0\u00bb0px||0px|30px|false|false\u00a0\u00bb border_width_left=\u00a0\u00bb1px\u00a0\u00bb border_color_left=\u00a0\u00bbgcid-primary-color\u00a0\u00bb locked=\u00a0\u00bboff\u00a0\u00bb global_colors_info=\u00a0\u00bb{%22gcid-primary-color%22:%91%22border_color_left%22%93}\u00a0\u00bb][et_pb_column type=\u00a0\u00bb4_4″ _builder_version=\u00a0\u00bb4.26.1″ _module_preset=\u00a0\u00bbdefault\u00a0\u00bb global_colors_info=\u00a0\u00bb{}\u00a0\u00bb][et_pb_text admin_label=\u00a0\u00bbTexte\u00a0\u00bb _builder_version=\u00a0\u00bb4.26.1″ _module_preset=\u00a0\u00bbdefault\u00a0\u00bb text_font=\u00a0\u00bb–et_global_body_font|500|||||||\u00a0\u00bb header_font=\u00a0\u00bb–et_global_body_font||||||||\u00a0\u00bb header_line_height=\u00a0\u00bb1.1em\u00a0\u00bb custom_margin=\u00a0\u00bb0px||15px||false|false\u00a0\u00bb custom_padding=\u00a0\u00bb0px||0px||true|false\u00a0\u00bb header_font_size_tablet=\u00a0\u00bb\u00a0\u00bb header_font_size_phone=\u00a0\u00bb38px\u00a0\u00bb header_font_size_last_edited=\u00a0\u00bbon|phone\u00a0\u00bb global_colors_info=\u00a0\u00bb{}\u00a0\u00bb]<\/p>\n

T\u00e9l\u00e9chargez la version d\u00e9mo de notre logiciel<\/h1>\n

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Vous avez la possibilit\u00e9 de t\u00e9l\u00e9charger la version d\u00e9mo de notre logiciel en cliquant sur le lien ci-dessous. Cette version vous permettra d’explorer ses fonctionnalit\u00e9s principales et de d\u00e9couvrir comment il peut r\u00e9pondre \u00e0 vos besoins.<\/p>\n

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Publications<\/h2>\n

[\/et_pb_text][\/et_pb_column][\/et_pb_row][et_pb_row _builder_version=\u00a0\u00bb4.26.1″ _module_preset=\u00a0\u00bbdefault\u00a0\u00bb custom_margin_tablet=\u00a0\u00bb\u00a0\u00bb custom_margin_phone=\u00a0\u00bb||0px||false|false\u00a0\u00bb custom_margin_last_edited=\u00a0\u00bbon|phone\u00a0\u00bb global_colors_info=\u00a0\u00bb{}\u00a0\u00bb][et_pb_column type=\u00a0\u00bb4_4″ _builder_version=\u00a0\u00bb4.26.1″ _module_preset=\u00a0\u00bbdefault\u00a0\u00bb global_colors_info=\u00a0\u00bb{}\u00a0\u00bb][et_pb_accordion toggle_icon=\u00a0\u00bb3||divi||400″ icon_color=\u00a0\u00bb#0a2d47″ use_icon_font_size=\u00a0\u00bbon\u00a0\u00bb icon_font_size=\u00a0\u00bb30px\u00a0\u00bb _builder_version=\u00a0\u00bb4.26.1″ _module_preset=\u00a0\u00bbdefault\u00a0\u00bb border_radii=\u00a0\u00bbon|20px|20px|20px|20px\u00a0\u00bb global_colors_info=\u00a0\u00bb{}\u00a0\u00bb][et_pb_accordion_item title=\u00a0\u00bbApplications aux satellites\u00a0\u00bb open=\u00a0\u00bbon\u00a0\u00bb open_toggle_text_color=\u00a0\u00bb#0a2d47″ closed_toggle_text_color=\u00a0\u00bb#0a2d47″ icon_color=\u00a0\u00bb#0a2d47″ use_icon_font_size=\u00a0\u00bbon\u00a0\u00bb icon_font_size=\u00a0\u00bb30px\u00a0\u00bb _builder_version=\u00a0\u00bb4.26.1″ _module_preset=\u00a0\u00bbdefault\u00a0\u00bb body_text_color=\u00a0\u00bb#0a2d47″ body_link_font=\u00a0\u00bb||||on|||#000000|\u00a0\u00bb body_link_text_color=\u00a0\u00bb#000000″ use_background_color_gradient=\u00a0\u00bbon\u00a0\u00bb background_color_gradient_direction=\u00a0\u00bb105deg\u00a0\u00bb background_color_gradient_stops=\u00a0\u00bbgcid-primary-color 0%|gcid-secondary-color 100%\u00a0\u00bb custom_padding=\u00a0\u00bb35px|35px|35px|35px|true|true\u00a0\u00bb global_colors_info=\u00a0\u00bb{%22gcid-primary-color%22:%91%22background_color_gradient_stops%22%93,%22gcid-secondary-color%22:%91%22background_color_gradient_stops%22%93}\u00a0\u00bb toggle_text_color=\u00a0\u00bb#0a2d47″ toggle_level=\u00a0\u00bbh3″ toggle_font_size=\u00a0\u00bb24px\u00a0\u00bb]<\/p>\n

Sanfedino, F., Alazard, D., Kiley, A., Watt, M., Simplicio, P., & Ankersen, F. (2023).\u00a0<\/span>Robust monolithic versus distributed control\/structure co-optimization of flexible space systems in presence of parametric uncertainties<\/a>.\u00a0ESA GNC 2023.<\/p>\n

Sanfedino, F., Thi\u00e9baud, G., Alazard, D., Guercio, N., & Deslaef, N. (2022).\u00a0<\/span>Advances in fine line-of-sight control for large space flexible structures<\/a>.\u00a0<\/span>Aerospace Science and Technology<\/em>,\u00a0<\/span>130<\/em>, 107961.<\/p>\n

Rodrigues, R., Preda, V., Sanfedino, F., & Alazard, D. (2022).\u00a0<\/span>Modeling, robust control synthesis and worst-case analysis for an on-orbit servicing mission with large flexible spacecraft<\/a>.\u00a0<\/span>Aerospace Science and Technology<\/em>, 107865.<\/p>\n

Sanfedino, F., Alazard, D., Preda, V., & Oddenino, D. (2022).\u00a0<\/span>Integrated modeling of microvibrations induced by Solar Array Drive Mechanism for worst-case end-to-end analysis and robust disturbance estimation<\/a>.\u00a0<\/span>Mechanical Systems and Signal Processing<\/em>,\u00a0<\/span>163<\/em>, 108168.<\/p>\n

Finozzi, A., Sanfedino, F., & Alazard, D. (2022).\u00a0<\/span>Parametric sub-structuring models of large space truss structures for structure\/control co-design<\/a>.\u00a0<\/span>Mechanical Systems and Signal Processing<\/em>,\u00a0<\/span>180<\/em>, 109427.<\/p>\n

Sanfedino, F., Preda, V., Pommier-Budinger, V., Alazard, D., Boquet, F., & Bennani, S. (2020).\u00a0<\/span>Robust active mirror control based on hybrid sensing for spacecraft line-of-sight stabilization<\/a>.\u00a0<\/span>IEEE Transactions on Control Systems Technology<\/em>,\u00a0<\/span>29<\/em>(1), 220-235.<\/p>\n

Sanfedino, F. (2019).\u00a0<\/span>Experimental validation of a high accuracy pointing system<\/a>\u00a0<\/span>(Doctoral dissertation, Toulouse, ISAE).<\/p>\n

Gonzalez, J. A. P., Pittet, C., Alazard, D., & Loquen, T. (2016).\u00a0<\/span>Integrated control\/structure design of a large space structure using structured hinfinity control<\/a>.\u00a0<\/span>IFAC-PapersOnLine<\/em>,\u00a0<\/span>49<\/em>(17), pp-296.<\/p>\n

Murali, H. H. S., Alazard, D., Massotti, L., Ankersen, F., & Toglia, C. (2015).\u00a0<\/span>Mechanical-attitude controller co-design of large flexible space structures<\/a>. In\u00a0<\/span>Advances in Aerospace Guidance, Navigation and Control<\/em>\u00a0<\/span>(pp. 659-678). Springer, Cham.<\/p>\n

Alazard, D., Loquen, T., De Plinval, H., & Cumer, C. (2013).\u00a0<\/span>Avionics\/Control co-design for large flexible space structures<\/a>. In\u00a0<\/span>AIAA Guidance, Navigation, and Control (GNC) Conference<\/em>\u00a0<\/span>(p. 4638).<\/p>\n

[\/et_pb_accordion_item][et_pb_accordion_item title=\u00a0\u00bbLa bo\u00eete \u00e0 outils SDTlib\u00a0\u00bb open_toggle_text_color=\u00a0\u00bb#0a2d47″ closed_toggle_text_color=\u00a0\u00bb#0a2d47″ icon_color=\u00a0\u00bb#0a2d47″ use_icon_font_size=\u00a0\u00bbon\u00a0\u00bb icon_font_size=\u00a0\u00bb30px\u00a0\u00bb _builder_version=\u00a0\u00bb4.26.1″ _module_preset=\u00a0\u00bbdefault\u00a0\u00bb body_text_color=\u00a0\u00bb#0a2d47″ body_link_font=\u00a0\u00bb||||on||||\u00a0\u00bb body_link_text_color=\u00a0\u00bb#000000″ use_background_color_gradient=\u00a0\u00bbon\u00a0\u00bb background_color_gradient_direction=\u00a0\u00bb105deg\u00a0\u00bb background_color_gradient_stops=\u00a0\u00bbgcid-primary-color 0%|gcid-secondary-color 100%\u00a0\u00bb custom_padding=\u00a0\u00bb35px|35px|35px|35px|true|true\u00a0\u00bb global_colors_info=\u00a0\u00bb{%22gcid-primary-color%22:%91%22background_color_gradient_stops%22%93,%22gcid-secondary-color%22:%91%22background_color_gradient_stops%22%93}\u00a0\u00bb toggle_text_color=\u00a0\u00bb#0a2d47″ toggle_level=\u00a0\u00bbh3″ toggle_font_size=\u00a0\u00bb24px\u00a0\u00bb open=\u00a0\u00bboff\u00a0\u00bb]<\/p>\n

Sanfedino, F., Alazard, D., Kassarian, E., & Somers, F. (2023).\u00a0<\/span>Satellite Dynamics Toolbox Library: a tool to model multi-body space systems for robust control synthesis and analysis<\/a>.\u00a0arXiv preprint arXiv:2303.15872<\/em>.<\/p>\n

Courie, I., Sanfedino, F., & Alazard, D. (2021).\u00a0<\/span>Worst-Case Pointing Performance Analysis for Large Flexible Spacecraft<\/a>.\u00a0<\/span>arXiv preprint arXiv:2106.01893<\/em>.<\/p>\n

Alazard, D., & Sanfedino, F. (2020, January).\u00a0<\/span>Satellite dynamics toolbox for preliminary design phase<\/a>. In\u00a0<\/span>43rd Annual AAS Guidance and Control Conference<\/em>\u00a0<\/span>(Vol. 30, pp. 1461-1472).<\/p>\n

Satellite Dynamics Toolbox library (SDTlib) \u2013\u00a0<\/span>User\u2019s Guide and tutoral\/demo version<\/a>.<\/p>\n

[\/et_pb_accordion_item][et_pb_accordion_item title=\u00a0\u00bbCadre th\u00e9orique\u00a0\u00bb open_toggle_text_color=\u00a0\u00bb#0a2d47″ closed_toggle_text_color=\u00a0\u00bb#0a2d47″ icon_color=\u00a0\u00bb#0a2d47″ use_icon_font_size=\u00a0\u00bbon\u00a0\u00bb icon_font_size=\u00a0\u00bb30px\u00a0\u00bb _builder_version=\u00a0\u00bb4.26.1″ _module_preset=\u00a0\u00bbdefault\u00a0\u00bb body_text_color=\u00a0\u00bb#0a2d47″ body_link_font=\u00a0\u00bb||||on|||#000000|\u00a0\u00bb body_link_text_color=\u00a0\u00bb#000000″ use_background_color_gradient=\u00a0\u00bbon\u00a0\u00bb background_color_gradient_direction=\u00a0\u00bb105deg\u00a0\u00bb background_color_gradient_stops=\u00a0\u00bbgcid-primary-color 0%|gcid-secondary-color 100%\u00a0\u00bb custom_padding=\u00a0\u00bb35px|35px|35px|35px|true|true\u00a0\u00bb global_colors_info=\u00a0\u00bb{%22gcid-primary-color%22:%91%22background_color_gradient_stops%22%93,%22gcid-secondary-color%22:%91%22background_color_gradient_stops%22%93}\u00a0\u00bb toggle_text_color=\u00a0\u00bb#0a2d47″ toggle_level=\u00a0\u00bbh3″ toggle_font_size=\u00a0\u00bb24px\u00a0\u00bb open=\u00a0\u00bboff\u00a0\u00bb]<\/p>\n

Alazard, D., Finozzi, A., & Sanfedino, F. (2023).\u00a0<\/span>Port inversions of parametric Two-Input Two-Output Port models of flexible substructures<\/a>.\u00a0Multibody System Dynamics<\/em>,\u00a057<\/em>(3-4), 365-387.<\/p>\n

Finozzi, A., Sanfedino, F., & Alazard, D. (2021).\u00a0<\/span>Analytical Port Inversion For A Flexible Model In The Two-Input Two-Output Port Approach<\/a>. In\u00a0<\/span>ECCOMAS Thematic Conference on Multibody Dynamics<\/em>\u00a0<\/span>(pp. 159-170). Budapest University of Technology and Economics.<\/p>\n

Sanfedino, F., Alazard, D., Pommier-Budinger, V., Falcoz, A., & Boquet, F. (2018).\u00a0<\/span>Finite element based N-Port model for preliminary design of multibody systems<\/a>.\u00a0<\/span>Journal of Sound and Vibration<\/em>,\u00a0<\/span>415<\/em>, 128-146.<\/p>\n

Chebbi, J., Dubanchet, V., Perez Gonzalez, J. A., & Alazard, D. (2017).\u00a0<\/span>Linear dynamics of flexible multibody systems<\/a>.\u00a0<\/span>Multibody System Dynamics<\/em>,\u00a0<\/span>41<\/em>(1), 75-100.<\/p>\n

Perez, J. A., Alazard, D., Loquen, T., Pittet, C., & Cumer, C. (2016).\u00a0<\/span>Flexible multibody system linear modeling for control using component modes synthesis and double-port approach<\/a>.\u00a0<\/span>Journal of Dynamic Systems, Measurement, and Control<\/em>,\u00a0<\/span>138<\/em>(12).<\/p>\n

Perez, J. A., Alazard, D., Loquen, T., Cumer, C., & Pittet, C. (2015).\u00a0<\/span>Linear dynamic modeling of spacecraft with open-chain assembly of flexible bodies for ACS\/structure co-design<\/a>. In\u00a0<\/span>Advances in aerospace guidance, navigation and control<\/em>\u00a0<\/span>(pp. 639-658). Springer, Cham.<\/p>\n

Alazard, D., Perez, J. A., Cumer, C., & Loquen, T. (2015).\u00a0<\/span>Two-input two-output port model for mechanical systems<\/a>. In\u00a0<\/span>AIAA Guidance, Navigation, and Control Conference<\/em>\u00a0<\/span>(p. 1778).<\/p>\n

Guy, N., Alazard, D., Cumer, C., & Charbonnel, C. (2014).\u00a0<\/span>Dynamic modeling and analysis of spacecraft with variable tilt of flexible appendages<\/a>.\u00a0<\/span>Journal of Dynamic Systems, Measurement, and Control<\/em>,\u00a0<\/span>136<\/em>(2), 021020.<\/p>\n

Tantawi, K. H., Alazard, D., & Cumer, C. (2008).\u00a0<\/span>Linear dynamic modeling of spacecraft with various flexible appendages<\/a>.\u00a0<\/span>IFAC Proceedings Volumes<\/em>,\u00a0<\/span>41<\/em>(2), 11148-11153.<\/p>\n

[\/et_pb_accordion_item][et_pb_accordion_item title=\u00a0\u00bbDynamique de type pendule multicorps\u00a0\u00bb open_toggle_text_color=\u00a0\u00bb#0a2d47″ closed_toggle_text_color=\u00a0\u00bb#0a2d47″ icon_color=\u00a0\u00bb#0a2d47″ use_icon_font_size=\u00a0\u00bbon\u00a0\u00bb icon_font_size=\u00a0\u00bb30px\u00a0\u00bb _builder_version=\u00a0\u00bb4.26.1″ _module_preset=\u00a0\u00bbdefault\u00a0\u00bb body_text_color=\u00a0\u00bb#0a2d47″ body_link_font=\u00a0\u00bb||||on||||\u00a0\u00bb body_link_text_color=\u00a0\u00bb#000000″ use_background_color_gradient=\u00a0\u00bbon\u00a0\u00bb background_color_gradient_direction=\u00a0\u00bb105deg\u00a0\u00bb background_color_gradient_stops=\u00a0\u00bbgcid-primary-color 0%|gcid-secondary-color 100%\u00a0\u00bb custom_padding=\u00a0\u00bb35px|35px|35px|35px|true|true\u00a0\u00bb global_colors_info=\u00a0\u00bb{%22gcid-primary-color%22:%91%22background_color_gradient_stops%22%93,%22gcid-secondary-color%22:%91%22background_color_gradient_stops%22%93}\u00a0\u00bb toggle_text_color=\u00a0\u00bb#0a2d47″ toggle_level=\u00a0\u00bbh3″ toggle_font_size=\u00a0\u00bb24px\u00a0\u00bb open=\u00a0\u00bboff\u00a0\u00bb]<\/p>\n

Kassarian, E., Sanfedino, F., Alazard, D., Montel, J., & Chevrier, C. A. (2023).\u00a0<\/span>Modeling of stratospheric balloons and robust line-of-sight pointing control<\/a>.\u00a0CEAS Space Journal<\/em>, 1-18.<\/p>\n

Kassarian, E., Sanfedino, F., Alazard, D., Montel, J., & Chevrier, C. A. (2022).\u00a0<\/span>Robust integrated control\/structure co-design for stratospheric balloons<\/a>.\u00a0<\/span>IFAC-PapersOnLine<\/em>,\u00a0<\/span>55<\/em>(25), 13-18.<\/p>\n

Kassarian, E., Sanfedino, F., Alazard, D., Chevrier, C. A., & Montel, J. (2022).\u00a0<\/span>Linear Fractional Transformation modeling of multibody dynamics around parameter-dependent equilibrium<\/a>.\u00a0<\/span>IEEE Transactions on Control Systems Technology<\/em>.<\/p>\n

Kassarian, E., Sanfedino, F., Alazard, D., Evain, H., & Montel, J. (2021).\u00a0<\/span>Modeling and stability of balloon-borne gondolas with coupled pendulum-torsion dynamics<\/a>.\u00a0Aerospace Science and Technology<\/em>,\u00a0112<\/em>, 106607.<\/p>\n

[\/et_pb_accordion_item][\/et_pb_accordion][\/et_pb_column][\/et_pb_row][\/et_pb_section]<\/p>\n","protected":false},"excerpt":{"rendered":"

T\u00e9l\u00e9chargez la version d\u00e9mo de notre logicielVous avez la possibilit\u00e9 de t\u00e9l\u00e9charger la version d\u00e9mo de notre logiciel en cliquant sur le lien ci-dessous. Cette version vous permettra d’explorer ses fonctionnalit\u00e9s principales et de d\u00e9couvrir comment il peut r\u00e9pondre \u00e0 vos besoins.Nos derniers articles

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Lorem ipsum dolor sit amet Consectetur adipiscing elit. Duis facilisis ornare magna, ac mattis justo viverra at. Proin a ex id arcu accumsan interdum quis a nunc. Donec a orci scelerisque purus euismod pretium non ac metus. Phasellus mauris lorem, tempor id pharetra nec, lobortis sit amet mauris. Cras<\/p>\n\t\t\t\t\t\t\t\t<\/div>\n\t\t\t\t\t\t\t<\/div>\n\t\t\t\t\t\t\t\n\t\t\t\t\t\t\t\t\n\t\t\t\t\t\t\t\t\t\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t\t\t<\/article>\n\n\t\t\t\t\n\t\t\t\t

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\n\t\t\t\t\t\t\t\t\t\t\t\n\t\t\t\t\t\t\t\t\t\t\t\tL\u2019approche TITOP pour la mod\u00e9lisation multicorps des structures flexibles\t\t\t\t\t\t\t\t\t\t\t<\/a>\n\t\t\t\t\t\t\t\t\t<\/h2>\n\t\t\t\t\t\t\t\t<\/header>\n\t\t\t\t\t\t\n\t\t\t\t\t\t\t\t\t\t\t\t\t
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