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Sanfedino, F., Alazard, D., Kiley, A., Watt, M., Simplicio, P., & Ankersen, F. (2023). <\/span>Robust monolithic versus distributed control\/structure co-optimization of flexible space systems in presence of parametric uncertainties<\/a>. ESA GNC 2023. <\/p>\n Sanfedino, F., Thi\u00e9baud, G., Alazard, D., Guercio, N., & Deslaef, N. (2022). <\/span>Advances in fine line-of-sight control for large space flexible structures<\/a>. <\/span>Aerospace Science and Technology<\/em>, <\/span>130<\/em>, 107961.<\/p>\n Rodrigues, R., Preda, V., Sanfedino, F., & Alazard, D. (2022). <\/span>Modeling, robust control synthesis and worst-case analysis for an on-orbit servicing mission with large flexible spacecraft<\/a>. <\/span>Aerospace Science and Technology<\/em>, 107865.<\/p>\n Sanfedino, F., Alazard, D., Preda, V., & Oddenino, D. (2022). <\/span>Integrated modeling of microvibrations induced by Solar Array Drive Mechanism for worst-case end-to-end analysis and robust disturbance estimation<\/a>. <\/span>Mechanical Systems and Signal Processing<\/em>, <\/span>163<\/em>, 108168.<\/p>\n Finozzi, A., Sanfedino, F., & Alazard, D. (2022). <\/span>Parametric sub-structuring models of large space truss structures for structure\/control co-design<\/a>. <\/span>Mechanical Systems and Signal Processing<\/em>, <\/span>180<\/em>, 109427.<\/p>\n Sanfedino, F., Preda, V., Pommier-Budinger, V., Alazard, D., Boquet, F., & Bennani, S. (2020). <\/span>Robust active mirror control based on hybrid sensing for spacecraft line-of-sight stabilization<\/a>. <\/span>IEEE Transactions on Control Systems Technology<\/em>, <\/span>29<\/em>(1), 220-235.<\/p>\n Sanfedino, F. (2019). <\/span>Experimental validation of a high accuracy pointing system<\/a> <\/span>(Doctoral dissertation, Toulouse, ISAE).<\/p>\n Gonzalez, J. A. P., Pittet, C., Alazard, D., & Loquen, T. (2016). <\/span>Integrated control\/structure design of a large space structure using structured hinfinity control<\/a>. <\/span>IFAC-PapersOnLine<\/em>, <\/span>49<\/em>(17), pp-296.<\/p>\n Murali, H. H. S., Alazard, D., Massotti, L., Ankersen, F., & Toglia, C. (2015). <\/span>Mechanical-attitude controller co-design of large flexible space structures<\/a>. In <\/span>Advances in Aerospace Guidance, Navigation and Control<\/em> <\/span>(pp. 659-678). Springer, Cham. <\/p>\n Alazard, D., Loquen, T., De Plinval, H., & Cumer, C. (2013). <\/span>Avionics\/Control co-design for large flexible space structures<\/a>. In <\/span>AIAA Guidance, Navigation, and Control (GNC) Conference<\/em> <\/span>(p. 4638).<\/p>\n [\/et_pb_accordion_item][et_pb_accordion_item title=”The SDTlib toolbox” open_toggle_text_color=”#0a2d47″ closed_toggle_text_color=”#0a2d47″ icon_color=”#0a2d47″ use_icon_font_size=”on” icon_font_size=”30px” _builder_version=”4.26.1″ _module_preset=”default” body_text_color=”#0a2d47″ body_link_font=”||||on||||” body_link_text_color=”#000000″ use_background_color_gradient=”on” background_color_gradient_direction=”105deg” background_color_gradient_stops=”gcid-primary-color 0%|gcid-secondary-color 100%” custom_padding=”35px|35px|35px|35px|true|true” global_colors_info=”{%22gcid-primary-color%22:%91%22background_color_gradient_stops%22%93,%22gcid-secondary-color%22:%91%22background_color_gradient_stops%22%93}” toggle_text_color=”#0a2d47″ toggle_level=”h3″ toggle_font_size=”24px” open=”off”]<\/p>\n Sanfedino, F., Alazard, D., Kassarian, E., & Somers, F. (2023). <\/span>Satellite Dynamics Toolbox Library: a tool to model multi-body space systems for robust control synthesis and analysis<\/a>. arXiv preprint arXiv:2303.15872<\/em>.<\/p>\n Courie, I., Sanfedino, F., & Alazard, D. (2021). <\/span>Worst-Case Pointing Performance Analysis for Large Flexible Spacecraft<\/a>. <\/span>arXiv preprint arXiv:2106.01893<\/em>.<\/p>\n Alazard, D., & Sanfedino, F. (2020, January). <\/span>Satellite dynamics toolbox for preliminary design phase<\/a>. In <\/span>43rd Annual AAS Guidance and Control Conference<\/em> <\/span>(Vol. 30, pp. 1461-1472).<\/p>\n Satellite Dynamics Toolbox library (SDTlib) – <\/span>User’s Guide and tutoral\/demo version<\/a>.<\/p>\n [\/et_pb_accordion_item][et_pb_accordion_item title=”Theoretical framework” open_toggle_text_color=”#0a2d47″ closed_toggle_text_color=”#0a2d47″ icon_color=”#0a2d47″ use_icon_font_size=”on” icon_font_size=”30px” _builder_version=”4.26.1″ _module_preset=”default” body_text_color=”#0a2d47″ body_link_font=”||||on|||#000000|” body_link_text_color=”#000000″ use_background_color_gradient=”on” background_color_gradient_direction=”105deg” background_color_gradient_stops=”gcid-primary-color 0%|gcid-secondary-color 100%” custom_padding=”35px|35px|35px|35px|true|true” global_colors_info=”{%22gcid-primary-color%22:%91%22background_color_gradient_stops%22%93,%22gcid-secondary-color%22:%91%22background_color_gradient_stops%22%93}” toggle_text_color=”#0a2d47″ toggle_level=”h3″ toggle_font_size=”24px” open=”off”]<\/p>\n Alazard, D., Finozzi, A., & Sanfedino, F. (2023). <\/span>Port inversions of parametric Two-Input Two-Output Port models of flexible substructures<\/a>. Multibody System Dynamics<\/em>, 57<\/em>(3-4), 365-387.<\/p>\n Finozzi, A., Sanfedino, F., & Alazard, D. (2021). <\/span>Analytical Port Inversion For A Flexible Model In The Two-Input Two-Output Port Approach<\/a>. In <\/span>ECCOMAS Thematic Conference on Multibody Dynamics<\/em> <\/span>(pp. 159-170). Budapest University of Technology and Economics. <\/p>\n Sanfedino, F., Alazard, D., Pommier-Budinger, V., Falcoz, A., & Boquet, F. (2018). <\/span>Finite element based N-Port model for preliminary design of multibody systems<\/a>. <\/span>Journal of Sound and Vibration<\/em>, <\/span>415<\/em>, 128-146.<\/p>\n Chebbi, J., Dubanchet, V., Perez Gonzalez, J. A., & Alazard, D. (2017). <\/span>Linear dynamics of flexible multibody systems<\/a>. <\/span>Multibody System Dynamics<\/em>, <\/span>41<\/em>(1), 75-100.<\/p>\n Perez, J. A., Alazard, D., Loquen, T., Pittet, C., & Cumer, C. (2016). <\/span>Flexible multibody system linear modeling for control using component modes synthesis and double-port approach<\/a>. <\/span>Journal of Dynamic Systems, Measurement, and Control<\/em>, <\/span>138<\/em>(12).<\/p>\n Perez, J. A., Alazard, D., Loquen, T., Cumer, C., & Pittet, C. (2015). <\/span>Linear dynamic modeling of spacecraft with open-chain assembly of flexible bodies for ACS\/structure co-design<\/a>. In <\/span>Advances in aerospace guidance, navigation and control<\/em> <\/span>(pp. 639-658). Springer, Cham. <\/p>\n Alazard, D., Perez, J. A., Cumer, C., & Loquen, T. (2015). <\/span>Two-input two-output port model for mechanical systems<\/a>. In <\/span>AIAA Guidance, Navigation, and Control Conference<\/em> <\/span>(p. 1778).<\/p>\n Guy, N., Alazard, D., Cumer, C., & Charbonnel, C. (2014). <\/span>Dynamic modeling and analysis of spacecraft with variable tilt of flexible appendages<\/a>. <\/span>Journal of Dynamic Systems, Measurement, and Control<\/em>, <\/span>136<\/em>(2), 021020.<\/p>\n Tantawi, K. H., Alazard, D., & Cumer, C. (2008). <\/span>Linear dynamic modeling of spacecraft with various flexible appendages<\/a>. <\/span>IFAC Proceedings Volumes<\/em>, <\/span>41<\/em>(2), 11148-11153.<\/p>\n [\/et_pb_accordion_item][et_pb_accordion_item title=”Multi-body pendulum dynamics” open_toggle_text_color=”#0a2d47″ closed_toggle_text_color=”#0a2d47″ icon_color=”#0a2d47″ use_icon_font_size=”on” icon_font_size=”30px” _builder_version=”4.26.1″ _module_preset=”default” body_text_color=”#0a2d47″ body_link_font=”||||on||||” body_link_text_color=”#000000″ use_background_color_gradient=”on” background_color_gradient_direction=”105deg” background_color_gradient_stops=”gcid-primary-color 0%|gcid-secondary-color 100%” custom_padding=”35px|35px|35px|35px|true|true” global_colors_info=”{%22gcid-primary-color%22:%91%22background_color_gradient_stops%22%93,%22gcid-secondary-color%22:%91%22background_color_gradient_stops%22%93}” toggle_text_color=”#0a2d47″ toggle_level=”h3″ toggle_font_size=”24px” open=”off”]<\/p>\n Kassarian, E., Sanfedino, F., Alazard, D., Montel, J., & Chevrier, C. A. (2023). <\/span>Modeling of stratospheric balloons and robust line-of-sight pointing control<\/a>. CEAS Space Journal<\/em>, 1-18.<\/p>\n Kassarian, E., Sanfedino, F., Alazard, D., Montel, J., & Chevrier, C. A. (2022). <\/span>Robust integrated control\/structure co-design for stratospheric balloons<\/a>. <\/span>IFAC-PapersOnLine<\/em>, <\/span>55<\/em>(25), 13-18.<\/p>\n Kassarian, E., Sanfedino, F., Alazard, D., Chevrier, C. A., & Montel, J. (2022). <\/span>Linear Fractional Transformation modeling of multibody dynamics around parameter-dependent equilibrium<\/a>. <\/span>IEEE Transactions on Control Systems Technology<\/em>.<\/p>\n Kassarian, E., Sanfedino, F., Alazard, D., Evain, H., & Montel, J. (2021). <\/span>Modeling and stability of balloon-borne gondolas with coupled pendulum-torsion dynamics<\/a>. Aerospace Science and Technology<\/em>, 112<\/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":" Download the demo version of our softwareYou can download the demo version of our software by clicking on the link below. This version will enable you to explore its main features and discover how it can meet your needs. Our latest articles\n\t\t\t\t\n\t\t\t\t\n\t\t\t\t\n\t\t\t\t\n\t\t\t\t\n\t\t\t\t\n\t\t\t\t\n\t\t\t\t\t\n\t\t\t\t\n\t\t\t\t\t\n\t\t\t\t\t\t\n\t\t\t\t\n\t\t\t\t\t\t\t\t\t\t\t\t\t\n\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t\n\t\t\t\t\t\t\t\t\t\n\t\t\t\t\t\t\t\t\t\t![\"\"](\"https:\/\/dycsyt.com\/wp-content\/uploads\/2024\/11\/themes.png\")
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