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			<title>The ION Group</title>
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				<title>The ION Group</title>
				<url>https://websites.isae-supaero.fr/local/cache-vignettes/L144xH30/rubon567-d262f.png?1775089142</url>
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		<title>Publications</title>
		<link>https://websites.isae-supaero.fr/the-ion-group/publications/publications</link>
		<guid isPermaLink="true">https://websites.isae-supaero.fr/the-ion-group/publications/publications</guid>
		<dc:date>2021-11-22T10:03:40Z</dc:date>
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		<dc:language>fr</dc:language>
		<dc:creator>c.morzadec</dc:creator>



		<description>
&lt;p&gt;[We have relocated our website !! Please visit instead ! This is an old website and soon will be turned off. &lt;br class='autobr' /&gt;
Journal Papers &lt;br class='autobr' /&gt;
LUSTOSA L.R., KOLMANOVSKY I., CESNIK C.E.S., VETRANO, F., Aided inertial estimation of wing shape. AIAA Journal of Guidance, Control, and Dynamics, Vol. 44, no. 2, 2021, pp. 210-219. &lt;br class='autobr' /&gt;
LUSTOSA L.R., DEFAY F., MOSCHETTA J.M., A global singularity-free aerodynamic model for algorithmic flight control of tail sitters. AIAA Journal of Guidance, Control, and Dynamics, (...)&lt;/p&gt;


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&lt;a href="https://websites.isae-supaero.fr/the-ion-group/publications/" rel="directory"&gt;Publications&lt;/a&gt;


		</description>


 <content:encoded>&lt;div class='rss_texte'&gt;&lt;p&gt;&lt;strong class=&#034;caractencadre-spip spip&#034;&gt;We have relocated our website !! Please visit &lt;a href=&#034;http://www.ionlab.fr&#034; class='spip_url spip_out' rel='external'&gt;www.ionlab.fr&lt;/a&gt; instead ! This is an old website and soon will be turned off.&lt;/strong&gt;&lt;/p&gt;
&lt;h3 class=&#034;spip&#034;&gt;Journal Papers&lt;/h3&gt;
&lt;p&gt;LUSTOSA L.R., KOLMANOVSKY I., CESNIK C.E.S., VETRANO, F., Aided inertial estimation of wing shape. AIAA Journal of Guidance, Control, and Dynamics, Vol. 44, no. 2, 2021, pp. 210-219.&lt;/p&gt;
&lt;p&gt;LUSTOSA L.R., DEFAY F., MOSCHETTA J.M., A global singularity-free aerodynamic model for algorithmic flight control of tail sitters. AIAA Journal of Guidance, Control, and Dynamics, Vol. 42, no. 2, 2019, pp. 303-316.&lt;/p&gt;
&lt;h3 class=&#034;spip&#034;&gt;Book Chapters&lt;/h3&gt;
&lt;p&gt;LUSTOSA L.R., WALDMANN J., A novel imaging measurement model for vision and inertial navigation fusion with extended Kalman filtering. Advances in estimation, navigation, and spacecraft control. 1ed Springer, 2015, v. 1, p. 275-289.&lt;/p&gt;
&lt;h3 class=&#034;spip&#034;&gt;Conferences&lt;/h3&gt;
&lt;p&gt;LUSTOSA L.R., CARDOSO-RIBEIRO F.L., DEFAY F., MOSCHETTA J.M., A new look at the uncontrollable linearized quaternion dynamics with implications to LQR design in underactuated systems. European Control Conference, 2018, Limassol, Cyprus.&lt;/p&gt;
&lt;p&gt;BARTH J.M.O., CONDOMINES J.P., BRONZ M., LUSTOSA L.R., MOSCHETTA J.M., JOIN C., FLIESS M., Fixed-wing UAV with transitioning flight capabilities : Model-based or model-free control approach ? A preliminary study. International Conference on Unmanned Aircraft Systems, 2018, Dallas, USA.&lt;/p&gt;
&lt;p&gt;LUSTOSA L.R., BARTH J.M.O., CONDOMINES J.P., DEFAY F., MOSCHETTA J.M., Team MAVion entry in the IMAV'17 outdoor challenge &#8212; A tail-sitting trajectory tracking MAV. International Micro Air Vehicle Conference and Competition, 2017, Toulouse, France.&lt;/p&gt;
&lt;p&gt;LUSTOSA L.R., DEFAY F., MOSCHETTA J.M., The feasibility issue in trajectory tracking by means of regions-of-attraction-based gain scheduling. IFAC 2017 World Congress, 2017, Toulouse, France.&lt;/p&gt;
&lt;p&gt;LUSTOSA L.R., PIZZIOL S., DEFAY F., MOSCHETTA J.M., An error model of a complementary filter for use in Bayesian estimation - The CF-EKF filter. 20th IFAC Symposium on Automatic Control in Aerospace, 2016, Sherbrooke, Canada.&lt;/p&gt;
&lt;p&gt;ALHERITIERE P.A., OLIVANTI R., LUSTOSA L.R., DEFAY F, MOSCHETTA J.M., Nonlinear control of a particular tilt-body MAV : The Roll and Fly. The 24th Mediterranean Conference on Control and Automation, 2016, Athens, Greece.&lt;/p&gt;
&lt;p&gt;LUSTOSA L.R., DEFAY F., MOSCHETTA J.M., Longitudinal study of a tilt-body vehicle : modeling, control and stability analysis. International Conference on Unmanned Aircraft Systems, 2015, Denver, USA.&lt;/p&gt;
&lt;p&gt;LUSTOSA L.R., DEFAY F., MOSCHETTA, J.M., Development of the flight model of a tilt-wing micro-air vehicle. International Micro Air Vehicle Conference and Competition, 2014, Delft, The Netherlands.&lt;/p&gt;
&lt;p&gt;MOSCHETTA J.M., LUSTOSA L.R., DEFAY F., On the design of hybrid micro air vehicles for multi-tasking missions. 2nd AETOS international conference on Research challenges for future RPAS/UAV systems, 2014, Bordeaux, France.&lt;/p&gt;
&lt;p&gt;LUSTOSA L.R., WALDMANN J., Addressing the statistical consistency of extended Kalman filtering for aided inertial navigation using adaptive techniques. ICINS2012 19th Saint Petersburg International Conference on Integrated Navigation Systems, 2012, Saint Petersburg, Russia.&lt;/p&gt;
&lt;p&gt;LUSTOSA L.R., WALDMANN J., A novel imaging measurement model for vision and inertial navigation fusion with extended Kalman filtering. Itzhack Y. Bar-Itzhack Memorial Symposium on Estimation, Navigation, and Spacecraft Control, 2012, Haifa, Israel.&lt;/p&gt;
&lt;p&gt;LUSTOSA L.R., CHAGAS R.A.J., WALDMANN J., Sighting device-aided inertial navigation : fusion with adaptive Kalman filtering techniques. COBEM 21st International Congress of Mechanical Engineering, 2011, Natal, Brazil.&lt;/p&gt;
&lt;p&gt;LUSTOSA L.R., BORGES G.A., Rastreamento de N alvos em movimento em sequ&#234;ncias de imagens para detec&#231;&#227;o de obst&#225;culos em rob&#243;tica m&#243;vel. 61a Reuni&#227;o Anual da Sociedade Brasileira para o Progresso da Ci&#234;ncia, 2009, Manaus, Brazil.&lt;/p&gt;&lt;/div&gt;
		
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				<item xml:lang="fr">
		<title>Projects</title>
		<link>https://websites.isae-supaero.fr/the-ion-group/projects/projects</link>
		<guid isPermaLink="true">https://websites.isae-supaero.fr/the-ion-group/projects/projects</guid>
		<dc:date>2021-11-22T10:03:32Z</dc:date>
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		<dc:language>fr</dc:language>
		<dc:creator>c.morzadec</dc:creator>



		<description>
&lt;p&gt;[We have relocated our website !! Please visit instead ! This is an old website and soon will be turned off. Towards satisfying strict power requirements in solar energy high-altitude pseudo-satellite aircraft, there's an increasing trend to optimize aerodynamic performance by increasing aspect ratio and to reduce weight by minimizing structure. Both solutions lead to increasingly flexible aircraft. Such potentially fragile systems call for protective control laws for managing load (...)&lt;/p&gt;


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&lt;a href="https://websites.isae-supaero.fr/the-ion-group/projects/" rel="directory"&gt;Projects&lt;/a&gt;


		</description>


 <content:encoded>&lt;div class='rss_texte'&gt;&lt;p&gt;&lt;strong class=&#034;caractencadre-spip spip&#034;&gt;We have relocated our website !! Please visit &lt;a href=&#034;http://www.ionlab.fr&#034; class='spip_url spip_out' rel='external'&gt;www.ionlab.fr&lt;/a&gt; instead ! This is an old website and soon will be turned off.&lt;/strong&gt;&lt;/p&gt;
&lt;hr class=&#034;spip&#034; /&gt;
&lt;p&gt;&lt;span class='spip_document_2893 spip_documents spip_documents_center'&gt;
&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L215xH29/halion-10557.png?1775089142' alt=&#034;&#034; class='ajustable' width='215' height='29' /&gt;&lt;/span&gt;&lt;/p&gt;
&lt;hr class=&#034;spip&#034; /&gt;
&lt;p&gt;&lt;span class='spip_document_2896 spip_documents spip_documents_left' style='float:left;'&gt;
&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L331xH141/jpoasa-e63f6.png?1775089142' alt=&#034;&#034; class='ajustable' width='331' height='141' /&gt;&lt;/span&gt; Towards satisfying strict power requirements in solar energy high-altitude pseudo-satellite aircraft, there's an increasing trend to optimize aerodynamic performance by increasing aspect ratio and to reduce weight by minimizing structure. Both solutions lead to increasingly flexible aircraft. Such potentially fragile systems call for protective control laws for managing load distribution during gusts and assure dynamic structural stability. The &lt;sc&gt;Halion&lt;/sc&gt; Project intends to study such control laws.&lt;/p&gt; &lt;iframe width=&#034;560&#034; height=&#034;315&#034; src=&#034;https://www.youtube.com/embed/sw59nTexvfk&#034; title=&#034;YouTube video player&#034; frameborder=&#034;0&#034; allow=&#034;accelerometer; autoplay; clipboard-write; encrypted-media; gyroscope; picture-in-picture&#034; allowfullscreen&gt;&lt;/iframe&gt; &lt;hr class=&#034;spip&#034; /&gt;
&lt;p&gt;&lt;span class='spip_document_2888 spip_documents spip_documents_center'&gt;
&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L189xH30/fusion-0d6e4.png?1775089142' alt=&#034;&#034; class='ajustable' width='189' height='30' /&gt;&lt;/span&gt;&lt;/p&gt;
&lt;hr class=&#034;spip&#034; /&gt;
&lt;p&gt;&lt;span class='spip_document_2902 spip_documents spip_documents_left' style='float:left;'&gt;
&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L134xH130/foguetedesenho-73994.png?1775089142' alt=&#034;&#034; class='ajustable' width='134' height='130' /&gt;&lt;/span&gt;This research task aims to study partially controllable systems (either by design or due to failure yielding degraded mode operation). A great example of such a problem is the automatic landing of non-throttleable rockets. While underactuated and not controllable, previous research in our group showed that landing is still possible in degraded mode at the expense of not choosing a precise touchdown location. Since partial controllability and the presence of strong non-linearities preclude linear control theory, the &lt;sc&gt;Fusion&lt;/sc&gt; Project pursues Nonlinear Model Predictive Control (NMPC) as a solution.&lt;/p&gt; &lt;iframe width=&#034;560&#034; height=&#034;315&#034; src=&#034;https://www.youtube.com/embed/5xCLp349sOQ&#034; title=&#034;YouTube video player&#034; frameborder=&#034;0&#034; allow=&#034;accelerometer; autoplay; clipboard-write; encrypted-media; gyroscope; picture-in-picture&#034; allowfullscreen&gt;&lt;/iframe&gt; &lt;hr class=&#034;spip&#034; /&gt;
&lt;p&gt;&lt;span class='spip_document_2895 spip_documents spip_documents_center'&gt;
&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L223xH43/mavion-af6a4.png?1775089142' alt=&#034;&#034; class='ajustable' width='223' height='43' /&gt;&lt;/span&gt;&lt;/p&gt;
&lt;hr class=&#034;spip&#034; /&gt;
&lt;p&gt;&lt;span class='spip_document_2904 spip_documents spip_documents_left' style='float:left;'&gt;
&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L219xH154/mavionsprite-7293a.png?1775089142' alt=&#034;&#034; class='ajustable' width='219' height='154' /&gt;&lt;/span&gt; This study sets out to establish tractable models for tail-sitting vehicles in view of control design and qualitative dynamics analysis. Our proposed framework not only yields numerically advantageous models but also extends our comprehension of tail-sitting vehicles. The proposed models are globally non-singular, polynomial-like and bypass the use of aerodynamic angles of attack and sideslip (both free-stream and propwash-induced !). Nevertheless, even if mathematically elegant, a mathematical model has practical use only if consistent with reality. This work shows this is the case by means of wind tunnel data and flight experiments.&lt;/p&gt; &lt;iframe width=&#034;560&#034; height=&#034;315&#034; src=&#034;https://www.youtube.com/embed/mzWiur1kS9s&#034; title=&#034;YouTube video player&#034; frameborder=&#034;0&#034; allow=&#034;accelerometer; autoplay; clipboard-write; encrypted-media; gyroscope; picture-in-picture&#034; allowfullscreen&gt;&lt;/iframe&gt; &lt;hr class=&#034;spip&#034; /&gt;
&lt;p&gt;&lt;span class='spip_document_2892 spip_documents spip_documents_center'&gt;
&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L165xH30/pilion-ea1db.png?1775089142' alt=&#034;&#034; class='ajustable' width='165' height='30' /&gt;&lt;/span&gt;&lt;/p&gt;
&lt;hr class=&#034;spip&#034; /&gt;
&lt;p&gt;Controllers and Observers are two sides of the same coin. The &lt;sc&gt;Pilion&lt;/sc&gt; Project delivers tailormade embedded system design for the above real-time tasks with artisan-like love and care.&lt;/p&gt;&lt;/div&gt;
		
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				<item xml:lang="fr">
		<title>People</title>
		<link>https://websites.isae-supaero.fr/the-ion-group/people/people</link>
		<guid isPermaLink="true">https://websites.isae-supaero.fr/the-ion-group/people/people</guid>
		<dc:date>2021-11-22T10:03:24Z</dc:date>
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		<dc:language>fr</dc:language>
		<dc:creator>c.morzadec</dc:creator>



		<description>
&lt;p&gt;[We have relocated our website !! Please visit instead ! This is an old website and soon will be turned off. &lt;br class='autobr' /&gt;
Director &lt;br class='autobr' /&gt; Prof. Leandro LUSTOSA leandro.lustosa [at] isae-supaero.fr Office : 11.048 ---- &lt;br class='autobr' /&gt;
PhD Candidates &lt;br class='autobr' /&gt; Francisco PEDROSA-REIS francisco.pedrosa-reis [at] isae-supaero.fr Office : 11.040 Thesis : Nonlinear Control of High Aspect Ratio Aircraft using Nonlinear Deformation Formulations (Halion) Interests : Flight Control Laws (ATA-22 and 27), Flight Dynamics and Handling (...)&lt;/p&gt;


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&lt;a href="https://websites.isae-supaero.fr/the-ion-group/people/" rel="directory"&gt;People&lt;/a&gt;


		</description>


 <content:encoded>&lt;div class='rss_texte'&gt;&lt;p&gt;&lt;strong class=&#034;caractencadre-spip spip&#034;&gt;We have relocated our website !! Please visit &lt;a href=&#034;http://www.ionlab.fr&#034; class='spip_url spip_out' rel='external'&gt;www.ionlab.fr&lt;/a&gt; instead ! This is an old website and soon will be turned off.&lt;/strong&gt;&lt;/p&gt;
&lt;h3 class=&#034;spip&#034;&gt;Director&lt;/h3&gt;
&lt;p&gt;&lt;span class='spip_document_2885 spip_documents spip_documents_left' style='float:left;'&gt;
&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L219xH126/leo-3b6c8.png?1775089142' alt=&#034;&#034; class='ajustable' width='219' height='126' /&gt;&lt;/span&gt; &lt;br class='autobr' /&gt;
Prof. Leandro LUSTOSA &lt;br class='autobr' /&gt;
leandro.lustosa [at] isae-supaero.fr&lt;br class='autobr' /&gt;
Office : 11.048&lt;/p&gt;
&lt;hr class=&#034;spip&#034; /&gt;&lt;hr class=&#034;spip&#034; /&gt;&lt;h3 class=&#034;spip&#034;&gt;PhD Candidates&lt;/h3&gt;
&lt;p&gt;&lt;span class='spip_document_2934 spip_documents spip_documents_left' style='float:left;'&gt;
&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L217xH125/chico-4b6c6.png?1775089142' alt=&#034;&#034; class='ajustable' width='217' height='125' /&gt;&lt;/span&gt;&lt;br class='autobr' /&gt;
Francisco PEDROSA-REIS&lt;br class='autobr' /&gt;
francisco.pedrosa-reis [at] isae-supaero.fr&lt;br class='autobr' /&gt;
Office : 11.040&lt;br class='autobr' /&gt;
Thesis : Nonlinear Control of High Aspect Ratio Aircraft using Nonlinear Deformation Formulations (&lt;sc&gt;Halion&lt;/sc&gt;)&lt;br class='autobr' /&gt;
Interests : Flight Control Laws (ATA-22 and 27), Flight Dynamics and Handling Qualities, Aircraft Systems and Modeling&lt;/p&gt;
&lt;hr class=&#034;spip&#034; /&gt;&lt;h3 class=&#034;spip&#034;&gt;MSc Students&lt;/h3&gt;
&lt;p&gt;&lt;span class='spip_document_2906 spip_documents spip_documents_left' style='float:left;'&gt;
&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L217xH125/emptyphoto-1953f.png?1775089142' alt=&#034;&#034; class='ajustable' width='217' height='125' /&gt;&lt;/span&gt;&lt;br class='autobr' /&gt;
Lynn DAHER&lt;br class='autobr' /&gt;
Major : Aerospace Systems and Control&lt;br class='autobr' /&gt;
Projects : Reusable Rocket Landing on Model Scale (&lt;sc&gt;Fusion&lt;/sc&gt;)&lt;br class='autobr' /&gt;
Interests :&lt;/p&gt;
&lt;hr class=&#034;spip&#034; /&gt;&lt;hr class=&#034;spip&#034; /&gt;
&lt;p&gt;&lt;span class='spip_document_2909 spip_documents spip_documents_left' style='float:left;'&gt;
&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L217xH125/rodriguez-c01ef.png?1775089142' alt=&#034;&#034; class='ajustable' width='217' height='125' /&gt;&lt;/span&gt;&lt;br class='autobr' /&gt;
Omar ELIZONDO-RODRIGUEZ&lt;br class='autobr' /&gt;
Major : Aerospace Systems and Control&lt;br class='autobr' /&gt;
Projects : Reusable Rocket Landing on Model Scale (&lt;sc&gt;Fusion&lt;/sc&gt;)&lt;br class='autobr' /&gt;
Interests : Design of High Speed Vehicles, Control of Autonomous Flying/Underwater Vehicles, Kinematic Analysis and Synthesis, Sustainable Manufacturing, Computer Graphics&lt;/p&gt;
&lt;hr class=&#034;spip&#034; /&gt;
&lt;p&gt;&lt;span class='spip_document_2908 spip_documents spip_documents_left' style='float:left;'&gt;
&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L217xH125/kota-b8124.png?1775089142' alt=&#034;&#034; class='ajustable' width='217' height='125' /&gt;&lt;/span&gt;&lt;br class='autobr' /&gt;
Deeksha KOTA&lt;br class='autobr' /&gt;
Major : Aerospace Systems and Control&lt;br class='autobr' /&gt;
Projects : Loose Flight Control Laws for Longer Endurance (&lt;sc&gt;Mermoz&lt;/sc&gt;)&lt;br class='autobr' /&gt;
Interests : Flight Dynamics, Flight Control Laws, Sustainable Aviation&lt;/p&gt;
&lt;hr class=&#034;spip&#034; /&gt;&lt;hr class=&#034;spip&#034; /&gt;
&lt;p&gt;&lt;span class='spip_document_2915 spip_documents spip_documents_left' style='float:left;'&gt;
&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L214xH123/rohan-d70b1.png?1775089142' alt=&#034;&#034; class='ajustable' width='214' height='123' /&gt;&lt;/span&gt;&lt;br class='autobr' /&gt;
Rohan DHANSOIA&lt;br class='autobr' /&gt;
Major : Aerospace Systems and Control&lt;br class='autobr' /&gt;
Projects : Loose Flight Control Laws for Longer Endurance (&lt;sc&gt;Mermoz&lt;/sc&gt;)&lt;br class='autobr' /&gt;
Interests : MIMO Control, System Identification and Analysis, Optimization.&lt;/p&gt;
&lt;hr class=&#034;spip&#034; /&gt;&lt;hr class=&#034;spip&#034; /&gt;
&lt;p&gt;&lt;span class='spip_document_2922 spip_documents spip_documents_left' style='float:left;'&gt;
&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L215xH124/lana-6c802.png?1775089142' alt=&#034;&#034; class='ajustable' width='215' height='124' /&gt;&lt;/span&gt;&lt;br class='autobr' /&gt;
Lanna KUBA&lt;br class='autobr' /&gt;
Major : Aerospace Systems and Control&lt;br class='autobr' /&gt;
Projects : Reusable Rocket Landing on Model Scale (&lt;sc&gt;Fusion&lt;/sc&gt;)&lt;br class='autobr' /&gt;
Interests : Control Theory, System Identification and Analysis, Space Systems, Applied Mathematics, Green Aviation, Sustainable and environmentally friendly manufacturing methods.&lt;/p&gt;
&lt;hr class=&#034;spip&#034; /&gt;&lt;hr class=&#034;spip&#034; /&gt;
&lt;p&gt;&lt;span class='spip_document_2911 spip_documents spip_documents_left' style='float:left;'&gt;
&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L216xH124/yacine-471da.png?1775089142' alt=&#034;&#034; class='ajustable' width='216' height='124' /&gt;&lt;/span&gt;&lt;br class='autobr' /&gt;
Yacine BEN-BELKACEM&lt;br class='autobr' /&gt;
Major : Embedded Systems&lt;br class='autobr' /&gt;
Projects : Reusable Rocket Landing on Model Scale (&lt;sc&gt;Fusion&lt;/sc&gt;)&lt;br class='autobr' /&gt;
Interests : Robotics, Multi-body Systems Dynamics, Control Theory, Aerial Vehicles, Real-Time Embedded Systems.&lt;/p&gt;
&lt;hr class=&#034;spip&#034; /&gt;&lt;hr class=&#034;spip&#034; /&gt;
&lt;p&gt;&lt;span class='spip_document_2926 spip_documents spip_documents_left' style='float:left;'&gt;
&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L215xH124/menon-a72b4.png?1775089142' alt=&#034;&#034; class='ajustable' width='215' height='124' /&gt;&lt;/span&gt;&lt;br class='autobr' /&gt;
Aditya MENON&lt;br class='autobr' /&gt;
Major : Embedded Systems&lt;br class='autobr' /&gt;
Projects : In-Flight Wing Shape Estimator Design (&lt;sc&gt;Halion&lt;/sc&gt;)&lt;br class='autobr' /&gt;
Interests :&lt;/p&gt;
&lt;hr class=&#034;spip&#034; /&gt;&lt;hr class=&#034;spip&#034; /&gt;
&lt;p&gt;&lt;span class='spip_document_2924 spip_documents spip_documents_left' style='float:left;'&gt;
&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L215xH124/umer-be747.png?1775089142' alt=&#034;&#034; class='ajustable' width='215' height='124' /&gt;&lt;/span&gt;&lt;br class='autobr' /&gt;
Umer Naeem KHAN&lt;br class='autobr' /&gt;
Major : Embedded Systems&lt;br class='autobr' /&gt;
Project : In-Flight Wing Shape Estimator Design (&lt;sc&gt;Halion&lt;/sc&gt;)&lt;br class='autobr' /&gt;
Interests : Computer Vision, Aircraft Flight Dynamics, Machine Learning, and Smart Mobility.&lt;/p&gt;
&lt;hr class=&#034;spip&#034; /&gt;&lt;hr class=&#034;spip&#034; /&gt;
&lt;p&gt;&lt;span class='spip_document_2939 spip_documents spip_documents_left' style='float:left;'&gt;
&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L216xH125/shreyank-cdcdc.png?1775089142' alt=&#034;&#034; class='ajustable' width='216' height='125' /&gt;&lt;/span&gt;&lt;br class='autobr' /&gt;
Shreyank JOIS&lt;br class='autobr' /&gt;
Major : Embedded Systems&lt;br class='autobr' /&gt;
Project : Reconstructing the Apollo 11 Guidance Navigation and Control System (&lt;sc&gt;Pilion&lt;/sc&gt;)&lt;br class='autobr' /&gt;
Interests : Guidance Navigation and Control, Computational Fluid Dynamics, Real-time Computer Graphics.&lt;/p&gt;
&lt;hr class=&#034;spip&#034; /&gt;&lt;hr class=&#034;spip&#034; /&gt;
&lt;p&gt;&lt;span class='spip_document_2906 spip_documents spip_documents_left' style='float:left;'&gt;
&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L217xH125/emptyphoto-1953f.png?1775089142' alt=&#034;&#034; class='ajustable' width='217' height='125' /&gt;&lt;/span&gt;&lt;br class='autobr' /&gt;
Shafeequr REHMAN&lt;br class='autobr' /&gt;
Major : Aerospace Systems and Control&lt;br class='autobr' /&gt;
Project : Nonlinear Modeling and Control of a VTOL Vehicle (in collab. with &lt;sc&gt;TIDAV&lt;/sc&gt;)&lt;br class='autobr' /&gt;
Interests : System Modeling, Robust Control, Guidance, and Navigation.&lt;/p&gt;
&lt;hr class=&#034;spip&#034; /&gt;&lt;hr class=&#034;spip&#034; /&gt;&lt;/div&gt;
		
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		<title>Open positions</title>
		<link>https://websites.isae-supaero.fr/the-ion-group/open-positions/open-positions</link>
		<guid isPermaLink="true">https://websites.isae-supaero.fr/the-ion-group/open-positions/open-positions</guid>
		<dc:date>2021-11-22T10:03:07Z</dc:date>
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		<dc:creator>c.morzadec</dc:creator>



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&lt;p&gt;We have relocated our website!! Please visit www.ionlab.fr instead! This is an old website and soon will be turned off. &lt;br class='autobr' /&gt;
Open positions in our group are posted and updated here in real-time! This means that if a rolling-basis position is available here, it has not yet been filled. To apply for any of these positions, please email Leandro Lustosa with the required application. Please follow the application instructions to the letter to be considered. For MSc student projects, you must (...)&lt;/p&gt;


-
&lt;a href="https://websites.isae-supaero.fr/the-ion-group/open-positions/" rel="directory"&gt;Open positions&lt;/a&gt;


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 <content:encoded>&lt;div class='rss_texte'&gt;&lt;p&gt;&lt;strong class=&#034;caractencadre-spip spip&#034;&gt;We have relocated our website!! Please visit &lt;a href=&#034;http://www.ionlab.fr&#034; class='spip_url spip_out' rel='external'&gt;www.ionlab.fr&lt;/a&gt; instead! This is an old website and soon will be turned off.&lt;/strong&gt;&lt;/p&gt;
&lt;p&gt;Open positions in our group are posted and updated here in real-time! This means that if a rolling-basis position is available here, it has not yet been filled. To apply for any of these positions, please email Leandro Lustosa with the required application. Please follow the application instructions &lt;strong&gt;to the letter&lt;/strong&gt; to be considered. For MSc student projects, you must already be admitted to a Master Program at ISAE-SUPAERO to be considered.&lt;/p&gt;
&lt;h3 class=&#034;spip&#034;&gt;Open PhD Candidate Position!!&lt;/h3&gt;
&lt;p&gt;We are looking for talented Ph.D. candidates in Control Systems! Our group is prototyping an exciting and challenging new avionics concept for high-altitude pseudo-satellite aircraft. Want to help us out? More info below.&lt;/p&gt; &lt;dl class='spip_document_2932 spip_documents spip_documents_center'&gt;
&lt;dt&gt;&lt;a href='https://websites.isae-supaero.fr/IMG/pdf/phd-call-for-candidates.pdf' title='PDF - 259.1&#160;kb' type=&#034;application/pdf&#034;&gt;&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L52xH52/pdf-39070.png?1775040851' width='52' height='52' alt='PDF - 259.1&#160;kb' /&gt;&lt;/a&gt;&lt;/dt&gt;
&lt;/dl&gt;
&lt;/div&gt;
		
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		<title>Home</title>
		<link>https://websites.isae-supaero.fr/the-ion-group/home/home</link>
		<guid isPermaLink="true">https://websites.isae-supaero.fr/the-ion-group/home/home</guid>
		<dc:date>2021-11-19T08:35:24Z</dc:date>
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		<dc:language>fr</dc:language>
		<dc:creator>c.morzadec</dc:creator>



		<description>
&lt;p&gt;We have relocated our website !! Please visit www.ionlab.fr instead ! This is an old website and soon will be turned off. &lt;br class='autobr' /&gt;
Welcome to our group website ! Our upbeat and offbeat group aims to beat a bit of the hard dynamic systems problems around us. We are passionate about everything Guidance, Navigation and Control related.&lt;/p&gt;


-
&lt;a href="https://websites.isae-supaero.fr/the-ion-group/home/" rel="directory"&gt;Home&lt;/a&gt;


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 <content:encoded>&lt;div class='rss_texte'&gt;&lt;p&gt;&lt;strong class=&#034;caractencadre-spip spip&#034;&gt;We have relocated our website !! Please visit &lt;a href=&#034;http://www.ionlab.fr&#034; class='spip_url spip_out' rel='external'&gt;www.ionlab.fr&lt;/a&gt; instead ! This is an old website and soon will be turned off.&lt;/strong&gt;&lt;/p&gt;
&lt;p&gt;Welcome to our group website ! Our upbeat and offbeat group aims to beat a bit of the hard dynamic systems problems around us. We are passionate about everything Guidance, Navigation and Control related.&lt;/p&gt;
&lt;p&gt;&lt;span class='spip_document_2928 spip_documents spip_documents_center'&gt;
&lt;img src='https://websites.isae-supaero.fr/local/cache-vignettes/L495xH124/support-97ce4.png?1775089142' alt=&#034;&#034; class='ajustable' width='495' height='124' /&gt;&lt;/span&gt;&lt;/p&gt;&lt;/div&gt;
		
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