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<raweb xmlns:xlink="http://www.w3.org/1999/xlink" xml:lang="en" year="2016">
  <identification id="mctao" isproject="true">
    <shortname>MCTAO</shortname>
    <projectName>Mathematics for Control, Transport and Applications</projectName>
    <theme-de-recherche>Optimization and control of dynamic systems</theme-de-recherche>
    <domaine-de-recherche>Applied Mathematics, Computation and Simulation</domaine-de-recherche>
    <urlTeam>http://team.inria.fr/mctao/</urlTeam>
    <structure_exterieure type="Labs">
      <libelle>Institut Mathématique de Bourgogne</libelle>
    </structure_exterieure>
    <structure_exterieure type="Labs">
      <libelle>Laboratoire Jean-Alexandre Dieudonné (JAD)</libelle>
    </structure_exterieure>
    <structure_exterieure type="Organism">
      <libelle>CNRS</libelle>
    </structure_exterieure>
    <structure_exterieure type="Organism">
      <libelle>Université Nice - Sophia Antipolis</libelle>
    </structure_exterieure>
    <structure_exterieure type="Organism">
      <libelle>Université de Bourgogne</libelle>
    </structure_exterieure>
    <header_dates_team>Creation of the Team: 2012 January 01, updated into Project-Team: 2013 January 01</header_dates_team>
    <LeTypeProjet>Project-Team</LeTypeProjet>
    <keywordsSdN>
      <term>5.10.3. - Planning</term>
      <term>5.10.4. - Robot control</term>
      <term>6.1. - Mathematical Modeling</term>
      <term>6.1.1. - Continuous Modeling (PDE, ODE)</term>
      <term>6.1.4. - Multiscale modeling</term>
      <term>6.2.1. - Numerical analysis of PDE and ODE</term>
      <term>6.2.6. - Optimization</term>
      <term>6.4. - Automatic control</term>
      <term>6.4.1. - Deterministic control</term>
      <term>6.4.3. - Observability and Controlability</term>
      <term>6.4.4. - Stability and Stabilization</term>
    </keywordsSdN>
    <keywordsSecteurs>
      <term>2.6. - Biological and medical imaging</term>
      <term>5.2.3. - Aviation</term>
      <term>5.2.4. - Aerospace</term>
      <term>6.6. - Embedded systems</term>
    </keywordsSecteurs>
    <UR name="Sophia"/>
  </identification>
  <team id="uid1">
    <person key="mctao-2014-idp65552">
      <firstname>Jean-Baptiste</firstname>
      <lastname>Pomet</lastname>
      <categoryPro>Chercheur</categoryPro>
      <research-centre>Sophia</research-centre>
      <moreinfo>Team leader, Inria, Senior Researcher</moreinfo>
      <hdr>oui</hdr>
    </person>
    <person key="numed-2014-idp110504">
      <firstname>Laetitia</firstname>
      <lastname>Giraldi</lastname>
      <categoryPro>Chercheur</categoryPro>
      <research-centre>Sophia</research-centre>
      <moreinfo>Inria, Researcher</moreinfo>
    </person>
    <person key="mctao-2014-idp60264">
      <firstname>Bernard</firstname>
      <lastname>Bonnard</lastname>
      <categoryPro>Enseignant</categoryPro>
      <research-centre>Sophia</research-centre>
      <moreinfo>Univ. Bourgogne, Professor</moreinfo>
      <hdr>oui</hdr>
    </person>
    <person key="mctao-2014-idp64104">
      <firstname>Jean-Baptiste</firstname>
      <lastname>Caillau</lastname>
      <categoryPro>Enseignant</categoryPro>
      <research-centre>Sophia</research-centre>
      <moreinfo>Univ. Bourgogne, Professor,
on leave to Inria since September 1st</moreinfo>
      <hdr>oui</hdr>
    </person>
    <person key="mctao-2014-idp71048">
      <firstname>Ludovic</firstname>
      <lastname>Rifford</lastname>
      <categoryPro>Enseignant</categoryPro>
      <research-centre>Sophia</research-centre>
      <moreinfo>Univ. Nice, Professor</moreinfo>
      <hdr>oui</hdr>
    </person>
    <person key="mctao-2014-idp76312">
      <firstname>Zeinab</firstname>
      <lastname>Badreddine</lastname>
      <categoryPro>PhD</categoryPro>
      <research-centre>Sophia</research-centre>
      <moreinfo>Univ. Bourgogne, granted by Univ. Bourgogne</moreinfo>
    </person>
    <person key="mctao-2016-idp173456">
      <firstname>Alice</firstname>
      <lastname>Nolot</lastname>
      <categoryPro>PhD</categoryPro>
      <research-centre>Sophia</research-centre>
      <moreinfo>Univ. Bourgogne, granted by Univ. Bourgogne</moreinfo>
    </person>
    <person key="mctao-2015-idp72000">
      <firstname>Zheng</firstname>
      <lastname>Chen</lastname>
      <categoryPro>PhD</categoryPro>
      <research-centre>Sophia</research-centre>
      <moreinfo>Univ. Paris Saclay, until Sep 2016, granted by
Paris Saclay and Chinese Scholarship Council; now postdoc Univ. Toulouse</moreinfo>
    </person>
    <person key="mctao-2015-idp74600">
      <firstname>Michael</firstname>
      <lastname>Orieux</lastname>
      <categoryPro>PhD</categoryPro>
      <research-centre>Sophia</research-centre>
      <moreinfo>Univ. Paris IX, granted by ENS Cachan</moreinfo>
    </person>
    <person key="apics-2016-idp159888">
      <firstname>Sébastien</firstname>
      <lastname>Fueyo</lastname>
      <categoryPro>PhD</categoryPro>
      <research-centre>Sophia</research-centre>
      <moreinfo>Inria, half time with Project-Team APICS</moreinfo>
    </person>
    <person key="mctao-2014-idp67016">
      <firstname>Jérémy</firstname>
      <lastname>Rouot</lastname>
      <categoryPro>PhD</categoryPro>
      <research-centre>Sophia</research-centre>
      <moreinfo>Inria, until Nov 2016, granted by CNES and
région PACA; now postdoc at LAAS, Toulouse</moreinfo>
    </person>
    <person key="mctao-2015-idp77152">
      <firstname>Achille</firstname>
      <lastname>Sassi</lastname>
      <categoryPro>PhD</categoryPro>
      <research-centre>Sophia</research-centre>
      <moreinfo>Univ. Paris Saclay, granted by EADS-Astrium</moreinfo>
    </person>
    <person key="mctao-2015-idp78408">
      <firstname>Florentina</firstname>
      <lastname>Nicolau</lastname>
      <categoryPro>PostDoc</categoryPro>
      <research-centre>Sophia</research-centre>
      <moreinfo>Inria, granted by CNES,
until Aug 2016; now Faculty Member at ENSEA, Univ. Cergy-Pontoise</moreinfo>
    </person>
    <person key="athena-2014-idp70480">
      <firstname>Claire</firstname>
      <lastname>Senica</lastname>
      <categoryPro>Assistant</categoryPro>
      <research-centre>Sophia</research-centre>
      <moreinfo>Inria, part time</moreinfo>
    </person>
    <person key="mctao-2016-idp193504">
      <firstname>Michael</firstname>
      <lastname>Brunengo</lastname>
      <categoryPro>AutreCategorie</categoryPro>
      <research-centre>Sophia</research-centre>
      <moreinfo>Polytech Nice Sophia, stage M1, from Jun 2016 until Aug 2016</moreinfo>
    </person>
    <person key="mctao-2016-idp196016">
      <firstname>Yacine</firstname>
      <lastname>El Alaoui-Faris</lastname>
      <categoryPro>AutreCategorie</categoryPro>
      <research-centre>Sophia</research-centre>
      <moreinfo>ENSEEIHT, stage M1, from Jun 2016 until Sep 2016</moreinfo>
    </person>
    <person key="mctao-2016-idp198512">
      <firstname>Jaouad</firstname>
      <lastname>Essaydi</lastname>
      <categoryPro>AutreCategorie</categoryPro>
      <research-centre>Sophia</research-centre>
      <moreinfo>Polytech Nice Sophia, stage M1, from Jun 2016 until Aug 2016</moreinfo>
    </person>
    <person key="mctao-2016-idp201024">
      <firstname>Clément</firstname>
      <lastname>Moreau</lastname>
      <categoryPro>AutreCategorie</categoryPro>
      <research-centre>Sophia</research-centre>
      <moreinfo>ENS Cachan, stage M2, from Mar
2016 until Jul 2016</moreinfo>
    </person>
    <person key="mctao-2014-idp75056">
      <firstname>Thierry</firstname>
      <lastname>Dargent</lastname>
      <categoryPro>Visiteur</categoryPro>
      <research-centre>Sophia</research-centre>
      <moreinfo>Thales Alenia Space, Engineer</moreinfo>
    </person>
    <person key="mctao-2014-idp68352">
      <firstname>Joseph</firstname>
      <lastname>Gergaud</lastname>
      <categoryPro>Visiteur</categoryPro>
      <research-centre>Sophia</research-centre>
      <moreinfo>ENSEEIHT Toulouse, Professor</moreinfo>
      <hdr>oui</hdr>
    </person>
  </team>
  <presentation id="uid2">
    <bodyTitle>Overall Objectives</bodyTitle>
    <subsection id="uid3" level="1">
      <bodyTitle>Overall Objectives</bodyTitle>
      <p>The core endeavor of this team is to develop methods in control theory for finite-dimensional nonlinear systems, as well as in optimal transport,
and to be involved in real applications of these techniques.
Some mathematical fields like dynamical systems and optimal transport may benefit from control theory techniques.
Our primary domain of industrial applications will be space engineering, namely designing trajectories in space mechanics using optimal control and stabilization
techniques: transfer of a satellite between two Keplerian orbits,
rendez-vous problem, transfer of a satellite from the Earth to the
Moon or more complicated space missions.
A second field of applications is quantum control with applications to
Nuclear Magnetic Resonance and medical image processing.
A third and more recent one is the control of micro-swimmers,
i.e. swimming robots where the fluid-structure coupling has a very low
Reynolds number.</p>
    </subsection>
  </presentation>
  <fondements id="uid4">
    <bodyTitle>Research Program</bodyTitle>
    <subsection id="uid5" level="1">
      <bodyTitle>Control Systems</bodyTitle>
      <p>Our effort is directed toward efficient methods for the <i>control</i> of real (physical) systems, based on a <i>model</i> of the system to be controlled.
<i>System</i> refers to the physical plant or device, whereas <i>model</i> refers to a mathematical representation of it.</p>
      <p>We mostly investigate nonlinear systems whose nonlinearities admit a strong structure derived from physics; the
equations governing their behavior are then well known, and the modeling part consists in choosing what
phenomena are to be kept in the model used for control design, the other phenomena being treated as perturbations; a
more complete model may be used for simulations, for instance.
We focus on systems that admit a reliable finite-dimensional model, in continuous time; this means that models are
controlled ordinary differential equations, often nonlinear.</p>
      <p>Choosing accurate models yet simple enough to allow control design is in itself a key issue; however, modeling or identification as a theory is not per se in the scope of our project.</p>
      <p>The extreme generality and versatility of linear control do not contradict
the often heard sentence “most real life systems are nonlinear”.
Indeed, for many control problems, a linear model is sufficient to capture the important features for control.
The reason is that most
control objectives are local, first order variations around an operating point
or a trajectory are governed by a linear control model, and except in
degenerate situations (non-controllability of this linear
model), the local behavior of a nonlinear dynamic phenomenon is dictated by
the behavior of first order variations.
Linear control is the hard core of control theory and practice; it has been pushed to a high degree of achievement
–see for instance some classics: <ref xlink:href="#mctao-2016-bid0" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, <ref xlink:href="#mctao-2016-bid1" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>– that lead to big successes
in industrial applications (PID, Kalman filtering, frequency domain design,
<formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><msup><mi>H</mi><mi>∞</mi></msup></math></formula> robust control, etc...), it is taught to future engineers, and it is still a topic of ongoing research.</p>
      <p>Linear control by itself however reaches its limits in some important situations:</p>
      <orderedlist>
        <li id="uid6">
          <p noindent="true"><b>Non local control objectives.</b>
Steering the system
from a region to a reasonably remote other one, as in path planning
and optimal control, is outside the scope of information given by a local linear
approximation. It is why these are by essence nonlinear.</p>
          <p>Stabilisation with a basin of attraction larger than the region where
the linear approximation is dominant also needs more information than
one linear approximation.</p>
        </li>
        <li id="uid7">
          <p noindent="true"><b>Local control at degenerate equilibria.</b>
Linear control yields local stabilization of an equilibrium point based on
the tangent linear approximation if the latter is controllable. It is
<i>not</i> the case at interesting operating points of some physical
systems; linear control is irrelevant and specific nonlinear techniques have to be
designed.
This is an extreme case of the second part of the above item: the region where the linear approximation is dominant vanishes.</p>
        </li>
        <li id="uid8">
          <p noindent="true"><b>Small controls.</b> In some situations, actuators only allow a very small magnitude of the
effect of control compared to the effect of other phenomena. Then the behavior of the system without control plays a
major role and we are again outside the scope of linear control methods.</p>
        </li>
      </orderedlist>
    </subsection>
    <subsection id="uid9" level="1">
      <bodyTitle>Structure of nonlinear control systems </bodyTitle>
      <p>In most problems, choosing the proper coordinates, or the right quantities that describe a phenomenon, sheds
light on a path to the solution. In control systems, it is often crucial to analyze the structure of the
model, deduced from physical principles, of the plant to be controlled;
this may lead to putting it via some transformations in a simpler form, or a form that is
most suitable for control design.
For instance, equivalence to a linear system may allow to use linear control; also, the so-called “flatness” property drastically simplifies path planning  <ref xlink:href="#mctao-2016-bid2" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, <ref xlink:href="#mctao-2016-bid3" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>.</p>
      <p>A better understanding of the “set of nonlinear models”,
partly classifying them, has another motivation than facilitating control design for a given system and its model:
it may also be a necessary step towards a theory of “nonlinear identification” and modeling.
Linear identification is a mature area of control science;
its success is mostly due to a very fine knowledge of the structure of the class of linear models: similarly, any progress in
the understanding of the structure of the class of nonlinear models
would be a contribution to a possible theory of nonlinear
identification.</p>
      <p>These topics are central in control theory, but raise very difficult mathematical questions: static feedback
classification is a geometric problem which is feasible in principle, although describing invariants explicitly is
technically very difficult; and conditions for dynamic feedback equivalence and linearization raise unsolved
mathematical problems, that make one wonder about decidability <footnote id="uid10" id-text="1">Consider the simple system with state <formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><mrow><mrow><mo>(</mo><mi>x</mi><mo>,</mo><mi>y</mi><mo>,</mo><mi>z</mi><mo>)</mo></mrow><mo>∈</mo><mi>I</mi><mspace width="-0.166667em"/><mspace width="-0.166667em"/><msup><mi>R</mi><mn>3</mn></msup></mrow></math></formula> and two controls that reads
<formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><mrow><mover accent="true"><mi>z</mi><mo>˙</mo></mover><mo>=</mo><msup><mrow><mo>(</mo><mover accent="true"><mi>y</mi><mo>˙</mo></mover><mo>-</mo><mi>z</mi><mover accent="true"><mi>x</mi><mo>˙</mo></mover><mo>)</mo></mrow><mn>2</mn></msup><mover accent="true"><mi>x</mi><mo>˙</mo></mover></mrow></math></formula> after elimination of the controls; it is not known whether it is
equivalent to a linear system, or flat; this is because the property amounts to existence of a formula giving
the general solution as a function of two arbitrary functions of time and their derivatives up to a certain
order, but no bound on this order is known a priori, even for this very particular example.</footnote>.</p>
    </subsection>
    <subsection id="uid11" level="1">
      <bodyTitle>Optimal control and feedback control, stabilization</bodyTitle>
      <subsection id="uid12" level="2">
        <bodyTitle>Optimal control.</bodyTitle>
        <p>Mathematically speaking, optimal control is the modern branch of the calculus of variations, rather well established and
mature  <ref xlink:href="#mctao-2016-bid4" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, <ref xlink:href="#mctao-2016-bid5" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, <ref xlink:href="#mctao-2016-bid6" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, <ref xlink:href="#mctao-2016-bid7" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>.
Relying on Hamiltonian dynamics is now prevalent, instead of the standard Lagrangian formalism of the calculus of variations.
Also, coming from control engineering, constraints on the control (for instance the control is a force or a torque, which are naturally bounded) or the state (for example in the shuttle
atmospheric re-entry problem there is a constraint on the thermal flux) are imposed; the ones on the state are usual but
these on the state yield more complicated necessary optimality conditions and an increased intrinsic complexity of the optimal solutions. Also, in the modern treatment, ad-hoc numerical schemes have to be derived for effective computations of the optimal solutions.</p>
        <p>What makes optimal control an applied field is the necessity of computing these optimal trajectories, or rather the controls that produce these trajectories
(or, of course, close-by trajectories).
Computing a given optimal trajectory and its control as a function of time is a demanding task, with non trivial numerical difficulties: roughly speaking, the Pontryagin Maximum
Principle gives candidate optimal trajectories as solutions of a two point boundary value problem (for an ODE) which can be analyzed using mathematical tools from geometric control theory or solved numerically using shooting methods.
Obtaining the <i>optimal synthesis</i>
–the optimal control as a function of the state– is of course a more intricate problem  <ref xlink:href="#mctao-2016-bid6" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, <ref xlink:href="#mctao-2016-bid8" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>.</p>
        <p>These questions are not only academic for minimizing a cost is <i>very</i> relevant in many control engineering problems.
However, modern engineering textbooks in nonlinear control systems like the “best-seller” <ref xlink:href="#mctao-2016-bid9" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/> hardly mention optimal control, and rather put the emphasis on designing a feedback control,
as regular and explicit as possible, satisfying some qualitative (and extremely important!) objectives:
disturbance attenuation, decoupling, output regulation or stabilization.
Optimal control is sometimes viewed as disconnected from automatic
control... we shall come back to this unfortunate point.</p>
      </subsection>
      <subsection id="uid13" level="2">
        <bodyTitle>Feedback, control Lyapunov functions, stabilization.</bodyTitle>
        <p>A control Lyapunov function <b>(CLF)</b> is a function that can be
made a Lyapunov function (roughly speaking, a function that decreases
along all trajectories, some call this an “artificial potential”)
for the closed-loop system corresponding to <i>some</i> feedback law.
This can be translated into a partial differential relation sometimes
called “Artstein's (in)equation”  <ref xlink:href="#mctao-2016-bid10" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>.
There is a definite parallel between a CLF for
stabilization, solution of this differential inequation on the one
hand, and the value function of an optimal control problem for the
system, solution of a HJB equation on the other hand. Now, optimal
control is a quantitative objective while stabilization is a
qualitative objective; it is not surprising that Artstein (in)equation
is very under-determined and has many more solutions than HJB
equation, and that it may (although not always) even have smooth ones.</p>
        <p>We have, in the team, a longstanding research record on the topic of construction of CLFs and stabilizing feedback controls.</p>
      </subsection>
    </subsection>
    <subsection id="uid14" level="1">
      <bodyTitle>Optimal Transport</bodyTitle>
      <p>We believe that matching optimal transport with geometric control theory is one originality of our team. We expect
interactions in both ways.</p>
      <p>The study of optimal mass transport problems in the Euclidean or
Riemannian setting has a long history which goes from the pioneer
works of Monge  <ref xlink:href="#mctao-2016-bid11" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/> and Kantorovitch  <ref xlink:href="#mctao-2016-bid12" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/> to the
recent revival initiated by fundamental contributions due to Brenier  <ref xlink:href="#mctao-2016-bid13" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/> and McCann  <ref xlink:href="#mctao-2016-bid14" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>.</p>
      <p>The same transportation problems in the presence of
differential constraints on the set of paths —like being an admissible trajectory for a control system— is quite new. The first
contributors were Ambrosio and Rigot  <ref xlink:href="#mctao-2016-bid15" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/> who proved the
existence and uniqueness of an optimal transport map for the Monge
problem associated with the squared canonical sub-Riemannian distance on the Heisenberg groups. This
result was extended later by Agrachev and Lee  <ref xlink:href="#mctao-2016-bid16" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, then by Figalli and
Rifford  <ref xlink:href="#mctao-2016-bid17" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/> who showed that the Ambrosio-Rigot theorem
holds indeed true on many sub-Riemannian manifolds satisfying
reasonable assumptions.
The problem of existence and uniqueness of an optimal transport map for the squared sub-Riemannian distance on a
general complete sub-Riemannian manifold remains open; it is strictly related to the regularity of the sub-Riemannian
distance in the product space, and remains a formidable challenge.
Generalized notions of Ricci curvatures (bounded from below) in metric spaces have been developed recently by Lott and
Villani  <ref xlink:href="#mctao-2016-bid18" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/> and Sturm  <ref xlink:href="#mctao-2016-bid19" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>. A pioneer work by
Juillet  <ref xlink:href="#mctao-2016-bid20" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/> captured the right notion of curvature for
subriemannian metric in the Heisenberg group; Agrachev and
Lee  <ref xlink:href="#mctao-2016-bid21" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/> have elaborated on this work to define new
notions of curvatures in three dimensional sub-Riemannian
structures. The optimal transport approach happened to be very
fruitful in this context. Many things remain to be done in a more
general context.
</p>
    </subsection>
    <subsection id="uid15" level="1">
      <bodyTitle>Small controls and conservative systems, averaging</bodyTitle>
      <p>Using averaging techniques to study small perturbations of integrable Hamiltonian systems dates back to H. Poincaré or
earlier; it gives an approximation of the (slow) evolution of quantities that are
preserved in the non-perturbed system. It is very subtle in the case of multiple periods but more elementary in the
single period case, here it boils down to taking the average of the perturbation along each periodic orbit; see for
instance <ref xlink:href="#mctao-2016-bid22" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, <ref xlink:href="#mctao-2016-bid23" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>.</p>
      <p>When the “perturbation” is a control, these techniques may be used after deciding how the control will depend on
time and state and other quantities, for instance it may be used after applying the
Pontryagin Maximum Principle as in  <ref xlink:href="#mctao-2016-bid24" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, <ref xlink:href="#mctao-2016-bid25" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, <ref xlink:href="#mctao-2016-bid26" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, <ref xlink:href="#mctao-2016-bid27" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>.
Without deciding the control a priori, an “average control system” may be defined as in <ref xlink:href="#mctao-2016-bid28" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>.</p>
      <p>The focus is then on studying into details this simpler “averaged” problem, that can often be described by a Riemannian
metric for quadratic costs or by a Finsler metric for costs like minimum time.</p>
      <p>This line of research stemmed out of applications to space engineering, see section <ref xlink:href="#uid17" location="intern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>.
</p>
    </subsection>
  </fondements>
  <domaine id="uid16">
    <bodyTitle>Application Domains</bodyTitle>
    <subsection id="uid17" level="1">
      <bodyTitle>Space engineering, satellites, low thrust control</bodyTitle>
      <p>Space engineering is very demanding in terms of safe and
high-performance control laws (for instance optimal in terms of fuel consumption, because only a finite amount of fuel is onboard a satellite
for all its “life”). It is therefore prone to real industrial
collaborations.</p>
      <p>We are especially interested in trajectory control of space vehicles using their own propulsion devices, outside the atmosphere.
Here we discuss “non-local” control problems (in the sense of section <ref xlink:href="#uid5" location="intern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/> point <ref xlink:href="#uid6" location="intern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>): orbit transfer rather than station keeping; also we do not discuss attitude control.</p>
      <p>In the geocentric case,
a space vehicle is subject to</p>
      <p noindent="true">- gravitational forces, from one or more central bodies (the corresponding
acceleration is denoted by <formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><msub><mi>F</mi><mrow><mi> grav </mi><mo>.</mo></mrow></msub></math></formula> below),</p>
      <p noindent="true">- a thrust, the control, produced by a propelling
device; it is the <formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><mrow><mi>G</mi><mspace width="0.166667em"/><mi>u</mi></mrow></math></formula> term below; assume for simplicity that control in all
directions is allowed, <i>i.e.</i> <formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><mi>G</mi></math></formula> is an invertible matrix</p>
      <p noindent="true">- other “perturbating” forces (the corresponding acceleration is
denoted by <formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><msub><mi>F</mi><mn>2</mn></msub></math></formula> below; in simplified models, it is not present).
In position-velocity coordinates, its dynamics can be written as</p>
      <formula id-text="1" id="uid18" textype="equation" type="display">
        <math xmlns="http://www.w3.org/1998/Math/MathML" mode="display" overflow="scroll">
          <mrow>
            <mover accent="true">
              <mi>x</mi>
              <mo>¨</mo>
            </mover>
            <mspace width="4pt"/>
            <mspace width="0.277778em"/>
            <mo>=</mo>
            <mspace width="0.277778em"/>
            <mspace width="4pt"/>
            <msub>
              <mi>F</mi>
              <mrow>
                <mi> grav </mi>
                <mo>.</mo>
              </mrow>
            </msub>
            <mrow>
              <mo>(</mo>
              <mi>x</mi>
              <mo>,</mo>
              <mi>t</mi>
              <mo>)</mo>
            </mrow>
            <mspace width="0.277778em"/>
            <mo>+</mo>
            <mspace width="0.277778em"/>
            <msub>
              <mi>F</mi>
              <mn>2</mn>
            </msub>
            <mrow>
              <mo>(</mo>
              <mi>x</mi>
              <mo>,</mo>
              <mover accent="true">
                <mi>x</mi>
                <mo>˙</mo>
              </mover>
              <mo>,</mo>
              <mi>t</mi>
              <mo>)</mo>
            </mrow>
            <mspace width="0.277778em"/>
            <mo>+</mo>
            <mspace width="0.277778em"/>
            <mi>G</mi>
            <mrow>
              <mo>(</mo>
              <mi>x</mi>
              <mo>,</mo>
              <mover accent="true">
                <mi>x</mi>
                <mo>˙</mo>
              </mover>
              <mo>)</mo>
            </mrow>
            <mspace width="0.166667em"/>
            <mi>u</mi>
            <mspace width="0.277778em"/>
            <mo>,</mo>
            <mspace width="4pt"/>
            <mspace width="4pt"/>
            <mspace width="4pt"/>
            <mspace width="4pt"/>
            <mspace width="4pt"/>
            <mrow>
              <mo>∥</mo>
              <mi>u</mi>
              <mo>∥</mo>
            </mrow>
            <mo>≤</mo>
            <msub>
              <mi>u</mi>
              <mi> max </mi>
            </msub>
            <mo>.</mo>
          </mrow>
        </math>
      </formula>
      <p noindent="true">In the case of a single attracting central body (the earth) and in a geocentric frame, <formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><msub><mi>F</mi><mrow><mi> grav </mi><mo>.</mo></mrow></msub></math></formula> does not
depend on time, or consists of a main term that does not depend on time and smaller terms reflecting the action of the
moon or the sun, that depend on time.
The second term is often neglected in the design of the control at first sight; it contains terms like atmospheric drag
or solar pressure. <formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><mi>G</mi></math></formula> could also bear an explicit dependence on time (here we omit the variation of the mass, that
decreases proportionally to <formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><mrow><mo>∥</mo><mi>u</mi><mo>∥</mo></mrow></math></formula>.</p>
      <subsection id="uid19" level="2">
        <bodyTitle>Low thrust</bodyTitle>
        <p>Low thrust means that <formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><msub><mi>u</mi><mi> max </mi></msub></math></formula> is small, or more precisely that the maximum magnitude of <formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><mrow><mi>G</mi><mspace width="0.166667em"/><mi>u</mi></mrow></math></formula> is small
with respect to the one of <formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><msub><mi>F</mi><mrow><mi> grav </mi><mo>.</mo></mrow></msub></math></formula>
(but in general not compared to <formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><msub><mi>F</mi><mn>2</mn></msub></math></formula>).
Hence the influence of the control is very weak instantaneously, and
trajectories can only be significantly modified by accumulating the effect of
this low thrust on a long time. Obviously this is possible only because the
free system is somehow conservative.
This was “abstracted” in section <ref xlink:href="#uid15" location="intern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>.</p>
        <p><i>Why low thrust ?</i> The common principle to all propulsion devices is to eject particles, with
some relative speed with respect to the vehicle; conservation of momentum
then induces, from the point of view of the vehicle alone, an external force, the “thrust” (and a mass decrease).
Ejecting the same mass of particles with a higher relative speed
results in a proportionally higher thrust; this relative speed (specific impulse, <formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><msub><mi>I</mi><mrow><mi>s</mi><mi>p</mi></mrow></msub></math></formula>) is a
characteristic of the engine; the higher the
<formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><msub><mi>I</mi><mrow><mi>s</mi><mi>p</mi></mrow></msub></math></formula>, the smaller the mass of particles needed for the same change in the vehicle momentum.
Engines with a higher <formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><msub><mi>I</mi><mrow><mi>s</mi><mi>p</mi></mrow></msub></math></formula> are highly desirable
because, for the same maneuvers, they reduce the mass of "fuel" to be taken
on-board the satellite, hence leaving more room (mass) for the payload.
“Classical” chemical engines use combustion to eject particles, at a somehow limited speed even with very efficient fuel;
the more recent electric engines use a magnetic field to accelerate particles and eject them at a considerably higher speed;
however electrical power is limited (solar cells), and only a small amount of particles can be accelerated per unit of time,
inducing the limitation on thrust magnitude.</p>
        <p>Electric engines theoretically allow many more maneuvers with the same amount of particles, with the drawback that the instant
force is very small; sophisticated control design is necessary to circumvent this drawback. High thrust engines allow simpler control procedures because they almost allow instant maneuvers (strategies consist in a few burns
at precise instants).</p>
      </subsection>
      <subsection id="uid20" level="2">
        <bodyTitle>Typical problems</bodyTitle>
        <p>Let us mention two.</p>
        <simplelist>
          <li id="uid21">
            <p noindent="true"><i>Orbit transfer or rendez-vous</i>.
It is the classical problem of bringing a satellite to its operating position from the orbit where it is delivered by the launcher; for instance from a GTO orbit to the
geostationary orbit at a prescribed longitude (one says rendez-vous when the longitude, or the position on the orbit, is prescribed, and transfer if it is free). In equation
(<ref xlink:href="#uid18" location="intern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>) for the dynamics, <formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><msub><mi>F</mi><mrow><mi> grav </mi><mo>.</mo></mrow></msub></math></formula> is the Newtonian gravitation force of the earth (it then does not depend on time); <formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><msub><mi>F</mi><mn>2</mn></msub></math></formula> contains all the terms coming
either from the perturbations to the Newtonian potential or from external forces like radiation pressure, and the control is usually allowed in all directions, or with some
restrictions to be made precise.</p>
          </li>
          <li id="uid22">
            <p noindent="true"><i>Three body problem</i>.
This is about missions in the solar system leaving the region where the attraction of the earth, or another single body, is preponderant. We are then no longer in the
situation of a single central body, <formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><msub><mi>F</mi><mrow><mi> grav </mi><mo>.</mo></mrow></msub></math></formula> contains the attraction of different planets and the sun. In regions where two central bodies have an influence, say
the earth and the moon, or the sun and a planet, the term <formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><msub><mi>F</mi><mrow><mi> grav </mi><mo>.</mo></mrow></msub></math></formula> in (<ref xlink:href="#uid18" location="intern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>) is the one of the restricted three body problem and dependence on time
reflects the movement of the two “big” attracting bodies.</p>
            <p>An issue for future experimental missions in the solar system is interplanetary flight planning with gravitational assistance.
Tackling this global problem, that even contains some combinatorial problems (itinerary), goes beyond the methodology developed here, but the above considerations are a brick
in this puzzle.</p>
          </li>
        </simplelist>
      </subsection>
      <subsection id="uid23" level="2">
        <bodyTitle>Properties of the control system.</bodyTitle>
        <p>If there are no restrictions on the thrust direction, i.e., in equation (<ref xlink:href="#uid18" location="intern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>), if the control <formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><mi>u</mi></math></formula> has dimension 3 with an invertible matrix <formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><mi>G</mi></math></formula>, then the control system
is “static feedback linearizable”, and a fortiori flat, see section <ref xlink:href="#uid9" location="intern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>. However, implementing the static feedback transformation would consist in using the control to
“cancel” the gravitation; this is obviously impossible since the available thrust is very small.
As mentioned in section <ref xlink:href="#uid5" location="intern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, point <ref xlink:href="#uid8" location="intern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, the problem remains fully nonlinear in spite of this “linearizable” structure <footnote id="uid24" id-text="2">However, the linear approximation around <i>any</i> feasible trajectory is controllable (a periodic time-varying linear system);
optimal control problems will have no singular or abnormal trajectories.</footnote>.</p>
      </subsection>
    </subsection>
    <subsection id="uid25" level="1">
      <bodyTitle>Quantum Control</bodyTitle>
      <p>These applications started by a collaboration between B. Bonnard and
D. Sugny (a physicist from ICB) in the ANR project Comoc (now ended).
The problem was the control of the orientation of a molecule using a laser field, with a model that does take into account the dissipation due to the interaction with the
environment, molecular collisions for instance. The model is a dissipative generalization of the finite dimensional
Schrödinger equation, known as Lindblad equation.
It is a 3-dimensional system depending upon 3 parameters, yielding a very complicated optimal control problem that we have solved for prescribed boundary conditions.
In particular we have computed the minimum time control and the minimum energy control for the orientation or a
two-level system, using geometric optimal control and appropriate numerical methods (shooting and numerical continuation)  <ref xlink:href="#mctao-2016-bid29" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, <ref xlink:href="#mctao-2016-bid30" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>.</p>
      <p>More recently, based on this project, we have reoriented our control activity towards Nuclear Magnetic Resonance (MNR).
In MNR medical imaging, the contrast problem is the one of designing a variation of the magnetic field with respect to
time that maximizes the difference,
on the resulting image, between two different chemical species; this is the “contrast”. This research is conducted
with Prof. S. Glaser (TU-München), whose group is performing both in vivo and in vitro experiments;
experiments using our techniques have successfully measured the improvement in contrast between materials chemical
species that have an importance in medicine, like oxygenated and de-oxygenated blood,
see  <ref xlink:href="#mctao-2016-bid31" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>; this is however still to be investigated and improved.
The model is the Bloch equation for spin <formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><mfrac><mn>1</mn><mn>2</mn></mfrac></math></formula> particles, that can be interpreted as a sub-case of Lindblad equation
for a two-level system; the control problem to solve amounts to driving in minimum time the magnetization vector of the
spin to zero (for parameters of the system corresponding to one of the species), and generalizations where such
spin <formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><mfrac><mn>1</mn><mn>2</mn></mfrac></math></formula> particles are coupled: double spin inversion for instance.</p>
      <p>A reference book by B. Bonnard and D. Sugny has been published on the topic  <ref xlink:href="#mctao-2016-bid32" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>.</p>
    </subsection>
    <subsection id="uid26" level="1">
      <bodyTitle>Swimming at low-Reynolds number</bodyTitle>
      <p>The study of the swimming strategies of micro-organisms is attracting
increasing attention in the recent literature. This is both because of
the intrinsic biological interest, and for the possible implications
these studies may have on the design of bio-inspired artificial
replicas reproducing the functionalities of biological systems. In the
case of micro-swimmers, the surrounding fluid is dominated by the
viscosity effects of the water and becomes reversible. This feature,
known as the scallop theorem in that context needs to be circumvented
when one wants to swim with strokes that produce a net motion of the
swimmer. In this regime, it turns out that the dynamic of a
micro-swimmer could be expressed as an ordinary differential
equation. First of all, by stating that the swimmer controls its own
shape, we focus on finding the best strategy to swim (by minimizing a
time or an energy). Moreover, we work on the control and optimal
control of magnetic micro-swimmers. The latter micro-device is charged
in order to be deformed by an external magnetic field. In this case,
the control functions are the external magnetic field. And we wonder
whether it is possible to control the position of the swimmer by acting on this external magnetic field. We are also interested in the associated optimal control problem (acting on the magnetic field in such a way that the swimmer reaches a desired position as soon as possible).</p>
    </subsection>
    <subsection id="uid27" level="1">
      <bodyTitle>Applications of optimal transport</bodyTitle>
      <p>Optimal Transportation in general has many applications. Image processing, biology, fluid mechanics, mathematical
physics, game theory, traffic planning, financial mathematics, economics are among the most popular fields of
application of the general theory of optimal transport. Many developments have been made in all these fields recently.
Three more specific examples:</p>
      <p noindent="true">-
In image processing, since a grey-scale image may be viewed as a measure, optimal transportation has been used because
it gives a distance between measures corresponding to the optimal cost of moving densities from one to the other, see
e.g. the work of J.-M. Morel and co-workers  <ref xlink:href="#mctao-2016-bid33" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>.</p>
      <p noindent="true">-
In representation and approximation of
geometric shapes, say by point-cloud sampling, it is also interesting to associate a measure, rather than just a
geometric locus, to a distribution of points (this gives a small importance to exceptional “outlier” mistaken points);
this was developed in Q. Mérigot's PhD  <ref xlink:href="#mctao-2016-bid34" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/> in the GEOMETRICA project-team.
The relevant distance between measures is again the one coming from optimal transportation.</p>
      <p noindent="true">- The specific to the type of costs that we have considered in some
mathematical work, i.e. these coming from optimal control,
are concerned with evolutions of densities under state or velocity constraints. A fluid
motion or a crowd movement can be seen as the evolution of a density in a given space. If constraints are given on the
directions in which these densities can evolve, we are in the framework of non-holonomic transport problems.
</p>
    </subsection>
    <subsection id="uid28" level="1">
      <bodyTitle>Applications to some domains of mathematics. </bodyTitle>
      <p>Control theory (in particular thinking in terms of inputs and reachable set) has brought novel ideas and progresses to mathematics.
For instance, some problems from classical calculus of variations have been revisited in terms of optimal control and Pontryagin's Maximum Principle  <ref xlink:href="#mctao-2016-bid35" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>; also, closed geodesics for perturbed Riemannian metrics where constructed in  <ref xlink:href="#mctao-2016-bid36" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, <ref xlink:href="#mctao-2016-bid37" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/> using control techniques.</p>
      <p>Inside McTAO,
a work like <ref xlink:href="#mctao-2016-bid38" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, <ref xlink:href="#mctao-2016-bid39" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/> is definitely in this line, applying
techniques from control to construct some perturbations under constraints of Hamiltonian systems to solve longstanding
open questions in the field of dynamical systems.</p>
    </subsection>
  </domaine>
  <logiciels id="uid29">
    <bodyTitle>New Software and Platforms</bodyTitle>
    <subsection id="uid30" level="1">
      <bodyTitle>Hampath</bodyTitle>
      <p><span class="smallcap" align="left">Keywords:</span> Geometric control - Second order conditions - Differential homotopy - Ordinary differential equations</p>
      <p noindent="true">
        <span class="smallcap" align="left">Functional Description</span>
      </p>
      <p>Hampath is an open-source software developed to solve optimal control
problems by coupling shooting and homotopy methods. More generally, it can be used to
solve general Hamiltonian boudary value problems.
It also implements an efficient computation of Jacobi fields (allowing in particular
second order optimality condition checks) based on the repeated use of automatic
differentiation.</p>
      <simplelist>
        <li id="uid31">
          <p noindent="true">Participants: Jean-Baptiste Caillau, Olivier Cots and Joseph Gergaud</p>
        </li>
        <li id="uid32">
          <p noindent="true">Contact: Oliver Cots</p>
        </li>
        <li id="uid33">
          <p noindent="true">URL: <ref xlink:href="http://www.hampath.org" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">http://<allowbreak/>www.<allowbreak/>hampath.<allowbreak/>org</ref></p>
        </li>
      </simplelist>
    </subsection>
  </logiciels>
  <resultats id="uid34">
    <bodyTitle>New Results</bodyTitle>
    <subsection id="uid35" level="1">
      <bodyTitle>Advances in optimal control</bodyTitle>
      <subsection id="uid36" level="2">
        <bodyTitle>Algebraic and geometric techniques in medical resonance imaging</bodyTitle>
        <participants>
          <person key="mctao-2014-idp60264">
            <firstname>Bernard</firstname>
            <lastname>Bonnard</lastname>
          </person>
          <person key="PASUSERID">
            <firstname>Jean-Charles</firstname>
            <lastname>Faugère</lastname>
            <moreinfo>EPI PolSys</moreinfo>
          </person>
          <person key="PASUSERID">
            <firstname>Alain</firstname>
            <lastname>Jacquemard</lastname>
            <moreinfo>Univ. de Bourgogne</moreinfo>
          </person>
          <person key="PASUSERID">
            <firstname>Mohab</firstname>
            <lastname>Safey El Din</lastname>
            <moreinfo>EPI PolSys</moreinfo>
          </person>
          <person key="PASUSERID">
            <firstname>Thibaut</firstname>
            <lastname>Verron</lastname>
            <moreinfo>EPI PolSys</moreinfo>
          </person>
        </participants>
        <p>In the framework of the ANR-DFG project Explosys (see Section <ref xlink:href="#uid56" location="intern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>) we use computer algebra methods
to analyze the controlled Bloch equations, modeling the contrast
problem in MRI. The problem boils down to analyzing the so called singular
extremals associated to the problem. Thanks to the linear dependance
of the problem with respect to the state variables and the relaxation
parameters the problem is algebraic and is equivalent to determining equilibrium
points and eigenvalues of the linearized system at such points together
with the algebraic classification of the surface associated to the
switches between bang and singular arcs. Preliminary results are described
in ISSAC paper <ref xlink:href="#mctao-2016-bid40" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/> using Grobner basis and stratifications of singularities
of determinantal varieties. This work was a part of T. Verron's PhD
and is continuing in particular with him (Post doc APO-ENSEEIHT).</p>
      </subsection>
      <subsection id="uid37" level="2">
        <bodyTitle>Local minima, second order conditions</bodyTitle>
        <participants>
          <person key="mctao-2014-idp64104">
            <firstname>Jean-Baptiste</firstname>
            <lastname>Caillau</lastname>
          </person>
          <person key="mctao-2015-idp72000">
            <firstname>Zheng</firstname>
            <lastname>Chen</lastname>
          </person>
          <person key="PASUSERID">
            <firstname>Yacine</firstname>
            <lastname>Chitour</lastname>
            <moreinfo>Univ. Paris-Sud</moreinfo>
          </person>
          <person key="PASUSERID">
            <firstname>Ariadna</firstname>
            <lastname>Farrés</lastname>
            <moreinfo>Univ. Barcelona</moreinfo>
          </person>
        </participants>
        <p>It is well known that the PMP gives necessary conditions for optimality, but curves satisfying this condition may be local minima or critical sadle points.
Roughly speaking, the PMP is a first order condition.
Higher order conditions give finer necessary conditions (and sufficient in some special cases), but they require differentiability that is not always satisfied when commutations occur.
Furthermore, these local conditions cannot distinguish local from global minima. In <ref xlink:href="#mctao-2016-bid41" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/> and <ref xlink:href="#mctao-2016-bid42" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, we make contributions respectively to extending higher order conditions to non-smooth cases and to exploring local and global minima on an example of interest.</p>
        <p>Second order systems whose drift is defined by the gradient of a given potential are
considered, and minimization of the L<formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><msup><mrow/><mn>1</mn></msup></math></formula>-norm of the control is
addressed in <ref xlink:href="#mctao-2016-bid41" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>. An analysis
of the extremal flow emphasizes the role of singular trajectories of order two <ref xlink:href="#mctao-2016-bid43" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, <ref xlink:href="#mctao-2016-bid44" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>; the case of the two-body potential is
treated in detail. In L<formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><msup><mrow/><mn>1</mn></msup></math></formula>-minimization, regular extremals are
associated with bang-bang controls (saturated ocnstraint on the norm); in order to assess their optimality properties, sufficient
conditions are given for broken extremals and related to the no-fold conditions of <ref xlink:href="#mctao-2016-bid45" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>. Two examples
of numerical verification of these conditions are proposed on a problem coming from
space mechanics.</p>
        <p>In another direction, we have been studying the structure of local minima for time minimization in the controlled three-body
problem. In <ref xlink:href="#mctao-2016-bid42" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, several homotopies are systematically used to unfold the structure
of these local minimizers, and the resulting singularity of the path associated with
the value function is analyzed numerically.</p>
      </subsection>
      <subsection id="uid38" level="2">
        <bodyTitle>Solving chance-constrained optimal control problems in aerospace engineering via Kernel Density Estimation</bodyTitle>
        <participants>
          <person key="mctao-2014-idp64104">
            <firstname>Jean-Baptiste</firstname>
            <lastname>Caillau</lastname>
          </person>
          <person key="PASUSERID">
            <firstname>Max</firstname>
            <lastname>Cerf</lastname>
            <moreinfo>Airbus Industries</moreinfo>
          </person>
          <person key="mctao-2015-idp77152">
            <firstname>Achille</firstname>
            <lastname>Sassi</lastname>
          </person>
          <person key="PASUSERID">
            <firstname>Emmanuel</firstname>
            <lastname>Trélat</lastname>
            <moreinfo>Univ. P. &amp; M. Curie</moreinfo>
          </person>
          <person key="PASUSERID">
            <firstname>Hasna</firstname>
            <lastname>Zidani</lastname>
            <moreinfo>ENSTA ParisTech</moreinfo>
          </person>
        </participants>
        <p>The goal of <ref xlink:href="#mctao-2016-bid46" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/> is to show how non-parametric statistics can be used to solve
chance-constrained optimization and optimal control problems by reformulating them
into deterministic ones, focusing on the details of the algorithmic approach. We use
the Kernel Density Estimation method to approximate the probability density function
of a random variable with unknown distribution, from a relatively small sample. In the
paper it is shown how this technique can be applied to a class of chance-constrained
optimization problem, focusing on the implementation of the method. In particular, in
our examples we analyze a chance-constrained version of the well known problem in
aerospace optimal control: the Goddard problem.
</p>
      </subsection>
    </subsection>
    <subsection id="uid39" level="1">
      <bodyTitle>Averaging and filtering for optimal control in Space mechanics</bodyTitle>
      <participants>
        <person key="mctao-2014-idp64104">
          <firstname>Jean-Baptiste</firstname>
          <lastname>Caillau</lastname>
        </person>
        <person key="mctao-2014-idp75056">
          <firstname>Thierry</firstname>
          <lastname>Dargent</lastname>
        </person>
        <person key="mctao-2015-idp78408">
          <firstname>Florentina</firstname>
          <lastname>Nicolau</lastname>
        </person>
        <person key="mctao-2014-idp65552">
          <firstname>Jean-Baptiste</firstname>
          <lastname>Pomet</lastname>
        </person>
        <person key="mctao-2014-idp67016">
          <firstname>Jérémy</firstname>
          <lastname>Rouot</lastname>
        </person>
      </participants>
      <p>Investigating averaging in optimal control for space mechanics with
low thrust, or more generally with conservative systems with “small”
controls is an ongoing subject in the team.
It is also central in the research contract with CNES mentioned in Section <ref xlink:href="#uid50" location="intern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>.</p>
      <subsection id="uid40" level="2">
        <bodyTitle>Convergence properties of the Maximum principle</bodyTitle>
        <p>Part of Jérémy Rouot's PhD <ref xlink:href="#mctao-2016-bid47" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/> was devoted to
convergence properties in the Hamiltonian system resulting from
Pontryagin's Maximum principle when the small parameter representing
the ratio between slow and fast velocities tends to zero.
The difference with previous work is that we give a clear method to
sort fast and slow variables in the adjoint variables, and we provide
convergence of these under some conditions.
A more complete publication is under preparation.</p>
      </subsection>
      <subsection id="uid41" level="2">
        <bodyTitle>Approximation by filtering in optimal control and
applications</bodyTitle>
        <p>Minimum time control of slow-fast systems is considered. In the case of only one fast
angle, averaging techniques are available for such systems. The approach introduced in
<ref xlink:href="#mctao-2016-bid48" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/> and <ref xlink:href="#mctao-2016-bid28" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/> is recalled, then extended to time dependent
systems by means of a suitable filtering operator. The process relies upon
approximating the dynamics by means of sliding windows. The size of these windows is
an additional parameter that provides intermediate approximations between averaging
over the whole fast angle period and the original dynamics. The method
was applied to problems coming from space mechanics, and is exposed in
<ref xlink:href="#mctao-2016-bid49" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>.</p>
      </subsection>
      <subsection id="uid42" level="2">
        <bodyTitle>Averaging with reconstruction of the fast variable</bodyTitle>
        <p>We have been studying a way to modify the initial condition of the
average equation in order to approach better (but in the mean) the
slow variable while reconstructing asymptotically the fast variable.
This follows an idea that was shown to work numerically in
<ref xlink:href="#mctao-2016-bid48" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>.</p>
        <p>In <ref xlink:href="#mctao-2016-bid50" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, we give a construction for Cauchy problems.
It is lighter than second order averaging, in that oscillating signals
and ODEs are not used, and still provides a second order error
<i>in the mean</i>, together with convergence of the fast variable.
This remains to be developed for two-point boundary value problems
like in optimal control.</p>
      </subsection>
    </subsection>
    <subsection id="uid43" level="1">
      <bodyTitle>Fully controlled slender microswimmers</bodyTitle>
      <subsection id="uid44" level="2">
        <bodyTitle>The <formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><mi>N</mi></math></formula>-link micro-swimmer</bodyTitle>
        <participants>
          <person key="PASUSERID">
            <firstname>François</firstname>
            <lastname>Alouges</lastname>
            <moreinfo>École Polytechnique</moreinfo>
          </person>
          <person key="PASUSERID">
            <firstname>Antonio</firstname>
            <lastname>Desimone</lastname>
            <moreinfo>SISSA Trieste</moreinfo>
          </person>
          <person key="numed-2014-idp110504">
            <firstname>Laetitia</firstname>
            <lastname>Giraldi</lastname>
          </person>
          <person key="PASUSERID">
            <firstname>Marta</firstname>
            <lastname>Zopello</lastname>
            <moreinfo>Univ. di Padova</moreinfo>
          </person>
        </participants>
        <p>We discussed a reduced model to compute the motion of slender swimmers which propel themselves by changing the curvature of their body. Our approach is based on the use of Resistive Force Theory for the evaluation of the viscous forces and torques exerted by the surrounding fluid, and on discretizing the kinematics of the swimmer by representing its body through an articulated chain of <formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><mi>N</mi></math></formula> rigid links capable of planar deformations.
The resulting system of ODEs, governing the motion of the swimmer, is easy to assemble and to solve, making our reduced model a valuable tool in the design and optimization of bio-inspired artificial microdevices.
We prove that the swimmer composed by almost 3 segments is controllable in the whole plane.
As a direct result, there exists an optimal swimming strategy to reach a desired configuration in minimum time.
Numerical experiments for in the case of the Purcell swimmer suggest
that the optimal strategy is periodic, namely a sequence of identical
strokes. Our results indicate that this candidate for an optimal
stroke, indeed gives a better displacement speed than the classical
Purcell stroke.</p>
        <p>This is presented in <ref xlink:href="#mctao-2016-bid51" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/> (accepted as a Book chapter in Multi-scale Models in Mechano and Tumor Biology: Modeling, Homogenization and Applications, Lecture Notes in Computational Science and Engineering. June 2016).</p>
      </subsection>
      <subsection id="uid45" level="2">
        <bodyTitle>Optimal periodic strokes for the Copepod and Purcell micro-swimmers</bodyTitle>
        <participants>
          <person key="PASUSERID">
            <firstname>Piernicola</firstname>
            <lastname>Bettiol</lastname>
            <moreinfo>Uni. Bretagne Ouest</moreinfo>
          </person>
          <person key="mctao-2014-idp60264">
            <firstname>Bernard</firstname>
            <lastname>Bonnard</lastname>
          </person>
          <person key="mctao-2016-idp173456">
            <firstname>Alice</firstname>
            <lastname>Nolot</lastname>
          </person>
          <person key="mctao-2014-idp67016">
            <firstname>Jérémy</firstname>
            <lastname>Rouot</lastname>
          </person>
        </participants>
        <p>We have analyzed the problem
of optimizing the efficiency of the displacement of two micro swimmers
with slender links, namely the following two models: the symmetric micro swimmer introduced
by Takagi (see <ref xlink:href="#mctao-2016-bid52" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>); this is a model to
describe the locomotion of the micro crustaceans named copepod,
and the historical three link Purcell swimmer. The problems are studied
in the framework of optimal control theory and SR geometry vs the
standard curvature control point of view. Our contributions are to
determine the optimal solutions combining geometric analysis and adapted
numerical scheme. In particular the nilpotent models introduced in
SR geometry allow to make a neat analysis of the problem of determining
optimal strokes with small amplitudes and numerical continuation methods
are then applied to compute more general stroke. This approach is
completely original in optimal control. Also necessary and sufficient
optimality conditions are applied to select the topology of optimal
strokes (simple loops) and to determine the optimal solution in both
cases. For the references see <ref xlink:href="#mctao-2016-bid53" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/> and <ref xlink:href="#mctao-2016-bid54" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>. Also
note that in collaboration with D. Takagi and M. Chyba this approach is
currently at the experimental level at the university of Hawaii using
a robot micro swimmer mimicking a copepod, see above. More theoretical
issues in relation with SR geometry are investigated in the framework
of A. Nolot's starting PhD (started August, 2016).
Other publication relating these advances are <ref xlink:href="#mctao-2016-bid55" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, <ref xlink:href="#mctao-2016-bid56" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, <ref xlink:href="#mctao-2016-bid57" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>.
</p>
      </subsection>
    </subsection>
    <subsection id="uid46" level="1">
      <bodyTitle>Modelization and Controllability of “Magneto-elastic” Micro-swimmers</bodyTitle>
      <participants>
        <person key="PASUSERID">
          <firstname>François</firstname>
          <lastname>Alouges</lastname>
          <moreinfo>École Polytechnique</moreinfo>
        </person>
        <person key="PASUSERID">
          <firstname>Antonio</firstname>
          <lastname>Desimone</lastname>
          <moreinfo>SISSA Trieste</moreinfo>
        </person>
        <person key="numed-2014-idp110504">
          <firstname>Laetitia</firstname>
          <lastname>Giraldi</lastname>
        </person>
        <person key="PASUSERID">
          <firstname>Pierre</firstname>
          <lastname>Lissy</lastname>
          <moreinfo>Univ. Paris Dauphine</moreinfo>
        </person>
        <person key="mctao-2016-idp201024">
          <firstname>Clément</firstname>
          <lastname>Moreau</lastname>
          <moreinfo>ENS Cachan and York University</moreinfo>
        </person>
        <person key="mctao-2014-idp65552">
          <firstname>Jean-Baptiste</firstname>
          <lastname>Pomet</lastname>
        </person>
        <person key="PASUSERID">
          <firstname>Marta</firstname>
          <lastname>Zopello</lastname>
          <moreinfo>Univ. di Padova</moreinfo>
        </person>
      </participants>
      <p>It is not realistic for <i>artificial</i> micro-swimmers built as
micro-robots, to have an actuator at each joint. A possibility is as follows: each
link of the swimmer bears is magnetized and the movement is controlled
via an exterior magnetic field. These models also bear an internal
elastic force, that can be modelled as a torsional spring at each
joint and tends to asymptotically restore the straight shape in the absence
of other forces.</p>
      <p>Control strategies for these models have been proved successful
numerically.
It can also be proved mathematically via
an asymptotic analysis that it is
possible to steer the swimmer along a chosen direction with some well
chosen oscillating magnetic field, provided some obstruction, like
symmetries, are avoided. This is exposed in
<ref xlink:href="#mctao-2016-bid58" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/> for a Purcell magnetic swimmer (3 links).</p>
      <p>For the smallest magneto-elastic micro-swimmer (2 links), we have been
able to prove a strong local controllability result (weaker than STLC) around the
straight position of the swimmer, again except for values of the
parameters that correspond to symmetries preventing controllability. This is exposed in
<ref xlink:href="#mctao-2016-bid59" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, and a note is under preparation, that
shows that STLC is indeed <i>not</i> satisfied.
This analysis is difficult because the straight position corresponds
to the equilibria but is very degenerate from the control point of view.</p>
      <p>To avoid this degeneracy, a possibility is to “twist” one of the torsional
springs so that the equilibria no longer occur for a straight shape. This is exposed in
<ref xlink:href="#mctao-2016-bid60" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/> for a 3-link magnetic microswimmer
(local controllability has not been proved for this system without the
twist).
A local partial controllability result around the equilibrium is
proved in that case and a constructive method to find the magnetic
field that allows the swimmer to move along a prescribed trajectory is
described.
</p>
    </subsection>
    <subsection id="uid47" level="1">
      <bodyTitle>Sub-Riemannian Geometry and Optimal Transport</bodyTitle>
      <participants>
        <person key="mctao-2014-idp76312">
          <firstname>Zeinab</firstname>
          <lastname>Badreddine</lastname>
        </person>
        <person key="PASUSERID">
          <firstname>André</firstname>
          <lastname>Belotto Da Silva</lastname>
          <moreinfo>University of Toronto</moreinfo>
        </person>
        <person key="mctao-2014-idp71048">
          <firstname>Ludovic</firstname>
          <lastname>Rifford</lastname>
        </person>
      </participants>
      <p>We have studied the Sard Conjecture and its link with the problem of existence and uniqueness of an optimal transport map for a cost given by the square of a sub-Riemannian distance. Given a totally non-holonomic distribution on a smooth manifold, the Sard Conjecture is concerned with the the size of the set of points that can be reached by singular horizontal paths starting from a same point. In the setting of rank-two distributions in dimension three, the Sard conjecture states that that set should be a subset of the so-called Martinet surface of 2-dimensional Hausdorff measure zero. In <ref xlink:href="#mctao-2016-bid61" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, A. Belotto da Silva and L. Rifford proved that the conjecture holds in the case where the Martinet surface is smooth. Moreover, they address the case of singular real-analytic Martinet surfaces and show that the result holds true under an assumption of non-transversality of the distribution on the singular set of the Martinet surface. The methods rely on the control of the divergence of vector fields generating the trace of the distribution on the Martinet surface and some techniques of resolution of singularities.
In a work in progress, the control on the divergence of this
"generating" vector field is the key ingredient used by Z. Badreddine to obtain results of existence and uniqueness of optimal transport map for rank-two distribution in dimension four.
</p>
    </subsection>
    <subsection id="uid48" level="1">
      <bodyTitle>Geometric Control and Dynamics</bodyTitle>
      <participants>
        <person key="PASUSERID">
          <firstname>Ayadi</firstname>
          <lastname>Lazrag</lastname>
        </person>
        <person key="mctao-2014-idp71048">
          <firstname>Ludovic</firstname>
          <lastname>Rifford</lastname>
        </person>
        <person key="PASUSERID">
          <firstname>Rafael</firstname>
          <lastname>Ruggiero</lastname>
          <moreinfo>PUC-RIO</moreinfo>
        </person>
      </participants>
      <p>Following <ref xlink:href="#mctao-2016-bid62" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, <ref xlink:href="#mctao-2016-bid39" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/> and <ref xlink:href="#mctao-2016-bid38" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, we apply techniques from geometric control to the study of perturbations of Hamiltonian flows. In <ref xlink:href="#mctao-2016-bid63" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, we prove a uniform Franks' lemma at second order for geodesic flows and apply the result in persistence theory.</p>
    </subsection>
  </resultats>
  <contrats id="uid49">
    <bodyTitle>Bilateral Contracts and Grants with Industry</bodyTitle>
    <subsection id="uid50" level="1">
      <bodyTitle>CNES - Inria - UB Contract</bodyTitle>
      <p>Contract number: 130777/00. Call Number:  R-S13/BS-005-012</p>
      <p>"Perturbations and
averaging for low thrust" (Poussée faible et moyennation).</p>
      <p noindent="true">Research contract between CNES and McTAO (both the Inria and
the Université de Bourgogne parts).
It runs for the period 2014-2017.
It concerns averaging techniques in orbit transfers around the earth while taking into account many perturbations of the main
force (gravity for the earth considered as circular).
The objective is to validate numerically and theoretically the approximations made by using averaging, and to propose
methods that refine the approximation.
It has co-funded the PhD thesis of Jeremy Rouot
<ref xlink:href="#mctao-2016-bid47" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/> (also co-funded by Région PACA) and
fully funded the postdoc of Florentina Nicolau
<ref xlink:href="#mctao-2016-bid50" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, <ref xlink:href="#mctao-2016-bid49" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>.
</p>
    </subsection>
  </contrats>
  <partenariat id="uid51">
    <bodyTitle>Partnerships and Cooperations</bodyTitle>
    <subsection id="uid52" level="1">
      <bodyTitle>Regional Initiatives</bodyTitle>
      <p>The PhD thesis of Jeremy Rouot
<ref xlink:href="#mctao-2016-bid47" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/> has been co-funded by Région PACA.
</p>
    </subsection>
    <subsection id="uid53" level="1">
      <bodyTitle>National Initiatives</bodyTitle>
      <subsection id="uid54" level="2">
        <bodyTitle>ANR</bodyTitle>
        <p><b><ref xlink:href="http://perso.ens-lyon.fr/marco.mazzucchelli/KAM-Faible/" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">Weak
KAM beyond Hamilton-Jacobi (WKBHJ)</ref>.</b>
Started 2013 (decision ANR-12-BS01-0020 of December 19, 2012), duration: 4 years.
L. Rifford is in the scientific committee.</p>
        <p><b><ref xlink:href="https://www.ljll.math.upmc.fr/trelat/SRGI.html" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">Sub-Riemannian Geometry and Interactions (SRGI)</ref>.</b>
Started 2015 (decision ANR-15-CE40-0018), duration: 4 years.
L. Rifford is a member.</p>
        <p><b><ref xlink:href="http://www.agence-nationale-recherche.fr/?Projet=ANR-16-CE40-0013" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">Intéractions Systèmes Dynamiques Équations d'Évolution et Contrôle (ISDEEC)</ref>.</b>
Started 2016 (decision ANR-16-CE40-0013), duration: 4 years.
L. Rifford is a member.</p>
      </subsection>
      <subsection id="uid55" level="2">
        <bodyTitle>Others</bodyTitle>
        <p>The McTAO team participates in the <ref xlink:href="http://gdrmoa.math.cnrs.fr" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">GdR MOA</ref>,
a CNRS network on Mathematics of Optimization and Applications.</p>
        <p noindent="true" spacebefore="10.0pt">PEPS project of <ref xlink:href="http://www.agence-maths-entreprises.fr" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">AMIES</ref> Labex,
"Dealing with exclusion constraints in orbital transfer" with
Thalès Alenia Space (PI J.-B. Caillau). This project funded two master internships
during summer 2016
(M. Brunengo and Y. El Alaoui Faris, co-supervised with T. Dargent from Thalès).</p>
        <p noindent="true" spacebefore="10.0pt"><ref xlink:href="https://www.fondation-hadamard.fr/fr/pgmo/presentation-pgmo" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">PGMO</ref>
grant (2016-2017) on "Metric approximation of minimizing trajectories and
applications" (PI J.-B. Caillau). This project involves colleagues from Université
Paris Dauphine and has funding for one year, including one intership (M2 level).</p>
        <p noindent="true" spacebefore="10.0pt">J.-B. Caillau is associate researcher of the team
<ref xlink:href="http://uma.ensta-paristech.fr/oc" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">Optimization &amp; Control</ref> at
ENSTA-Paristech and of the CNRS team
<ref xlink:href="http://apo.enseeiht.fr" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">Parallel Algorithms &amp; Optimization team</ref> at
ENSEEIHT, Univ. Toulouse.</p>
      </subsection>
    </subsection>
    <subsection id="uid56" level="1">
      <bodyTitle>European Initiatives</bodyTitle>
      <subsection id="uid57" level="2">
        <bodyTitle>Collaborations in European Programs, other than FP7 &amp; H2020</bodyTitle>
        <subsection id="uid58" level="3">
          <bodyTitle>Bilateral program with Portugal</bodyTitle>
          <sanspuceslist>
            <li id="uid59">
              <p noindent="true">Program: FCT (Fundação para a Ciência e a Tecnologia)</p>
            </li>
            <li id="uid60">
              <p noindent="true">Grant no. : PTDC/MAT-CAL/4334/2014</p>
            </li>
            <li id="uid61">
              <p noindent="true">Project title: "Extremal spectral quantities and related problems"</p>
            </li>
            <li id="uid62">
              <p noindent="true">Duration: 05/2016-05/2019</p>
            </li>
            <li id="uid63">
              <p noindent="true">Coordinator: P. Freitas (Univ. Lisbon)</p>
            </li>
            <li id="uid64">
              <p noindent="true">Team member involved: J.-B. Caillau</p>
            </li>
            <li id="uid65">
              <p noindent="true">Other partners: Univ. Lisbon, Univ. Luxembourg, Czech Nuclear Physics
Institute, Univ. Bern</p>
            </li>
            <li id="uid66">
              <p noindent="true">Link: <ref xlink:href="https://team.inria.fr/mctao/fct-project-extremal-spectral-quantities-and-related-problems-2016-2019" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">https://<allowbreak/>team.<allowbreak/>inria.<allowbreak/>fr/<allowbreak/>mctao/<allowbreak/>fct-project-extremal-spectral-quantities-and-related-problems-2016-2019</ref></p>
            </li>
          </sanspuceslist>
        </subsection>
        <subsection id="uid67" level="3">
          <bodyTitle>Bilateral program with Germany</bodyTitle>
          <sanspuceslist>
            <li id="uid68">
              <p noindent="true">Program: Projets de recherche collaborative-internationale ANR-DFG (Germany)</p>
            </li>
            <li id="uid69">
              <p noindent="true">Grant no. : ANR-14-CE35-0013-01; DFG-Gl 203/9-1</p>
            </li>
            <li id="uid70">
              <p noindent="true">Project title: “<b>Exploring the physical limits of spin systems (Explosys).</b>”</p>
            </li>
            <li id="uid71">
              <p noindent="true">Duration: 11/2014-10/2018</p>
            </li>
            <li id="uid72">
              <p noindent="true">Coordinator: D. Sugny (Univ. de Bourgogne) for France, Glaser (TU München) for Germany.</p>
            </li>
            <li id="uid73">
              <p noindent="true">Team member involved: Bernard Bonnard is in the (scientific committee).</p>
            </li>
            <li id="uid74">
              <p noindent="true">Other partners: TU München, Univ. de Bourgogne (IMB and UCB).</p>
            </li>
            <li id="uid75">
              <p noindent="true">This project involves specialists in physics and control theory in order to make important progresses in the use of spin dynamics, in particular for Magnetic Resonance Medical Imaging.</p>
            </li>
            <li id="uid76">
              <p noindent="true">Link: <ref xlink:href="http://www.agence-nationale-recherche.fr/fileadmin/aap/2014/selection/pa-2014-selection-franco-allemand-dfg.pdf" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">http://<allowbreak/>www.<allowbreak/>agence-nationale-recherche.<allowbreak/>fr/<allowbreak/>fileadmin/<allowbreak/>aap/<allowbreak/>2014/<allowbreak/>selection/<allowbreak/>pa-2014-selection-franco-allemand-dfg.<allowbreak/>pdf</ref></p>
            </li>
          </sanspuceslist>
        </subsection>
      </subsection>
    </subsection>
  </partenariat>
  <diffusion id="uid77">
    <bodyTitle>Dissemination</bodyTitle>
    <subsection id="uid78" level="1">
      <bodyTitle>Promoting Scientific Activities</bodyTitle>
      <subsection id="uid79" level="2">
        <bodyTitle>Scientific Events Organisation</bodyTitle>
        <subsection id="uid80" level="3">
          <bodyTitle>General Chair, Scientific Chair</bodyTitle>
          <p><ref xlink:href="http://team.inria.fr/mctao/cut-locus2016-bangkok" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">The cut locus: A bridge over differential geometry, optimal control and transport</ref>,
Bangkok, August 2016 (B. Bonnard, J.-B. Caillau, K. Kondo, L. Rifford, M. Tanaka).
The conference was organized with the support of the Thai KMITL University and
gathered 30 people mostly from Japan, Thailand and France.</p>
        </subsection>
        <subsection id="uid81" level="3">
          <bodyTitle>Member of the Organizing Committees</bodyTitle>
          <p noindent="true" spacebefore="10.0pt"><ref xlink:href="https://www.imj-prg.fr/spip.php?article72" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">Séminaire de géométrie
hamiltonienne</ref>, Paris 6 (J.-B. Caillau). Bi-mensual seminar.</p>
          <p noindent="true" spacebefore="10.0pt"><ref xlink:href="https://team.inria.fr/mctao/journee-equipe-mctao-inria-sophia-18012016" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">Journée McTAO</ref>,
Inria Sophia, January 2016. One day event organized by the team with four invited
speakers.</p>
          <p noindent="true" spacebefore="10.0pt"><ref xlink:href="http://gmcnet.webs.ull.es/?q=node/1396" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">10th International Young Researcher Workshop on Geometry, Mechanics and Control</ref>,
Paris (IHP), January 2016 (J.-B. Caillau). The workshop gathered 50 people for
conferences and mini-courses.</p>
          <p noindent="true" spacebefore="10.0pt"><ref xlink:href="https://mode2016.sciencesconf.org" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">Journées SMAI-MODE</ref>,
Toulouse, March 2016 (J.-B. Caillau). The conference
gathered 140 researchers, and was coupled with a series of two
mini-courses co-organized with <ref xlink:href="http://gdrmoa.math.cnrs.fr" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">GdR MOA</ref>.</p>
          <p noindent="true" spacebefore="10.0pt"><ref xlink:href="https://team.inria.fr/mctao/journees-mokatoa-equipes-mokaplan-et-mctao-3-et-4-octobre-2016-paris" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">Journée MokaTAO</ref>,
Inria Paris, October 2016. Two-day event co-organized by Mokaplan (Inria Paris) and
McTAO teams, with talks by members of these teams. The two teams share common interests in optimization and optimal
transportation.</p>
          <p noindent="true" spacebefore="10.0pt"><ref xlink:href="https://team.inria.fr/mctao/groupe-de-travail-optimisation-et-applications-18-novembre-2016-sophia" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">Groupe de travail "Optimisation et applications"</ref>, Inria Sophia Antipolis, November
2016 (J.-B. Caillau). One day event with four invited speakers.</p>
        </subsection>
      </subsection>
      <subsection id="uid82" level="2">
        <bodyTitle>Books</bodyTitle>
        <subsection id="uid83" level="3">
          <bodyTitle>Springer briefs</bodyTitle>
          <p noindent="true" spacebefore="10.0pt">B. Bonnard and J. Rouot, together with M. Chyba, have written the series of
notes <ref xlink:href="#mctao-2016-bid64" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, submitted as Springer briefsPublications. They were the basis
of courses at the Phd level given at the University of Burgundy and
at the institute of Mathematics for industry at Fukuoka (Japan)</p>
        </subsection>
        <subsection id="uid84" level="3">
          <bodyTitle>Springer Maths and Industry</bodyTitle>
          <p>B. Bonnard, together with M. Chyba, served as an editor of the volume <ref xlink:href="#mctao-2016-bid65" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>, which gather contributions on the
subject by specialists of both academics and space agencies.</p>
        </subsection>
        <subsection id="uid85" level="3">
          <bodyTitle>Radon Series on Comput. and Applied Math.</bodyTitle>
          <p>J.-B. Caillau, together with M. Bergounioux, G. Peyré, C. Schnörr and T. Haberkorn, served as an editor for the volume <ref xlink:href="#mctao-2016-bid66" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/>.
With a focus on the interplay between mathematics and applications of imaging, the
first part covers topics from optimization, inverse problems and shape spaces to
computer vision and computational anatomy. The second part is geared towards geometric
control and related topics, including Riemannian geometry, celestial mechanics and
quantum control.</p>
        </subsection>
      </subsection>
      <subsection id="uid86" level="2">
        <bodyTitle>Journals</bodyTitle>
        <subsection id="uid87" level="3">
          <bodyTitle>Member of the Editorial Boards</bodyTitle>
          <p>L. Rifford has been a member of the Editorial Board of the journal "Discrete and Continuous Dynamical Systems - A" since 2014.</p>
        </subsection>
        <subsection id="uid88" level="3">
          <bodyTitle>Reviewer - Reviewing Activities</bodyTitle>
          <p>The team members have reviewed articles in 2016 for the following journals:
SIAM J. Control &amp; Optim.,
ESAIM Control Optim. and Calc. Var.,
Automatica,
J. Dyn. Control Syst.,
J. Optim. Theory Appl.,
J. Math. Pures Appl.,
Inventiones Mathematicae,
Mathematische Zeitschrift,
Advances in Differential Equations,
Memoirs of the American Mathematical Society,
Annales Scientifiques de l'ENS,
Nonlinear Analysis,
Communications in Mathematical Physics</p>
        </subsection>
      </subsection>
      <subsection id="uid89" level="2">
        <bodyTitle>Invited Talks</bodyTitle>
        <p>J.-B. Caillau</p>
        <p noindent="true">03/2016: <i>Séminaire Géométrie et dynamique</i>, Nice</p>
        <p noindent="true">04/2016: <i>Séminaire de Géométrie hamiltonienne</i>, Paris</p>
        <p noindent="true">05/2016: <i>Emerging Trends in Applied Mathematics and Mechanics</i>, Perpignan</p>
        <p noindent="true">06/2016: <i>Alicante-Limoges-Elche Meeting on Optimization</i>, Cartagena</p>
        <p noindent="true">08/2016: <i>The cut locus: A bridge over differential geometry, optimal control and
transport</i>, Bangkok</p>
        <p noindent="true">09/2016: <i>Séminaire Astrogéo</i>, Observatoire de la côte d'azur, Sophia</p>
        <p noindent="true" spacebefore="10.0pt">L. Giraldi</p>
        <p noindent="true">11/2016: <i>Controllability and hysteresis</i>, Trento, Italie</p>
        <p noindent="true" spacebefore="10.0pt">L. Rifford</p>
        <p noindent="true">02/2016: <i>Rencontre d'Analyse Mathématique et ses Applications</i>, Ouargla (Algeria)</p>
        <p noindent="true">02/2016: <i>Séminaire de Calculs des Variations et EDP</i>, Aix-Marseille University</p>
        <p noindent="true">03/2016: <i>CIMPA Research School "Géométrie et Analyse"</i>, Abidjan (Ivory Coast)</p>
        <p noindent="true">03/2016: <i>Séminaire Bourbaki</i>, Institut Henri Poincaré, Paris</p>
        <p noindent="true">04/2016: <i>Colloquium de l'Institut de Mathématiques</i>, University of Neuchâtel (Switzerland)</p>
        <p noindent="true">04/2016: <i>International Conference of the GE2MI</i>, Hammamet (Tunisia)</p>
        <p noindent="true">05/2016: <i>Colloquium du Département de Mathématiques</i>, University of Orsay</p>
        <p noindent="true">05/2016:<i>Geometric control and sub-Riemannian geometry</i>, Course given at the University of Isfahan (Iran)</p>
        <p noindent="true">06/2016: <i>Analysis, Geometry, and Optimal Transport</i>, KIAS, Seoul (South Korea)</p>
        <p noindent="true">08/2016: <i>The cut locus</i>, KIMTL, Bangkok (Thailand)</p>
        <p noindent="true">11/2016: <i>Dynamical Systems Seminar</i>, ETH Zurich</p>
        <p noindent="true">11/2016: <i>Dynamics and Geometry Seminar</i>, University Nice Sophia Antipolis</p>
        <p noindent="true">12/2016: <i>Seminar of Hamiltonian Geometry</i>, Paris VI</p>
        <p noindent="true">12/2016: <i>2016 Analysis School in Benin</i>, IMPS, Benin</p>
      </subsection>
      <subsection id="uid90" level="2">
        <bodyTitle>Leadership within the Scientific Community</bodyTitle>
        <p noindent="true">J.-B. Caillau has been head of the
<ref xlink:href="http://smai.emath.fr/spip.php?article338" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">SMAI-MODE</ref> group (2014-2016),
the group on optimization of the
French Society for Applied and Industrial Mathematics.</p>
        <p>L. Rifford has been executive director of CIMPA since September 2016.</p>
      </subsection>
      <subsection id="uid91" level="2">
        <bodyTitle>Scientific Expertise</bodyTitle>
        <p>J.-B. Caillau is
member of the scientific
committees of the “<ref xlink:href="https://www.imcce.fr" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">Institut de Mécanique Céleste de Calcul des Éphémérides</ref>”
and of the
<ref xlink:href="http://calcul.math.cnrs.fr/spip.php?article79" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">GdR Calcul</ref>,
and corresponding member in Dijon for the Labex
<ref xlink:href="http://www.agence-maths-entreprises.fr" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">AMIES</ref>.</p>
        <p>J.-B. Pomet is a member of the steering committee of “C4PO”, a
structuring project of the IDEX UCA<sup><small>JEDI</small></sup>.</p>
      </subsection>
      <subsection id="uid92" level="2">
        <bodyTitle>Research Administration</bodyTitle>
        <p>J.-B. Caillau is the joint head of the CNRS team
<ref xlink:href="http://math.u-bourgogne.fr/spip.php?rubrique26" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">Statistique, Probabilités, Optimisation &amp; Contrôle</ref>
at the Math. Institute of Univ. Bourgogne &amp; Franche-Comté.</p>
        <p>J.-B. Pomet has been an elected member of the Inria Evaluation
Committee (commission d'évaluation) since 2014.</p>
      </subsection>
    </subsection>
    <subsection id="uid93" level="1">
      <bodyTitle>Teaching - Supervision - Juries</bodyTitle>
      <subsection id="uid94" level="2">
        <bodyTitle>Teaching</bodyTitle>
        <p>J.-B. Caillau has managed L1 math and the master of applied mathematics
(M2 <ref xlink:href="http://blog.u-bourgogne.fr/migs" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">MIGS</ref>)
of Univ. Bourgogne Franche-Comté (2014-2016). He has been a designated member
of the Conseil pédagogique du Département de Mathématiques at UBFC (2014-2016),
and of the Conseil de l'UFR Mathématiques &amp; Informatique at Univ. Paris I (2014-2016).
His teaching duties in 2016 include:</p>
        <sanspuceslist>
          <li id="uid95">
            <p noindent="true">Licence : cours d'analyse (analysis), 100 H équivalent TD, niveau L1, Univ. Bourgogne
Franche-Comté, France</p>
          </li>
          <li id="uid96">
            <p noindent="true">Master : approximation géométrique (geometric approximation), 50 H équivalent TD, niveau
M1, Univ. Bourgogne Franche-Comté, France</p>
          </li>
          <li id="uid97">
            <p noindent="true">Master : optimisation, 50 H équivalent TD, niveau M2,
Univ. Bourgogne Franche-Comté, France</p>
          </li>
          <li id="uid98">
            <p noindent="true">Master : contrôle optimal (optimal control), 20 H équivalent TD, niveau M2,
ENSTA-Paristech, France</p>
          </li>
        </sanspuceslist>
        <p>L. Giraldi is responsible of the following courses:</p>
        <sanspuceslist>
          <li id="uid99">
            <p noindent="true">Licence : <i>“colles de mathématiques”, MPSI and MP</i>, 4 H équivalent TD/week, L1 L2, Lycée International de Valbonne,</p>
          </li>
          <li id="uid100">
            <p noindent="true">Licence : numerical analysis, 20 H équivalent TD, L3, Polytech Nice Sophia,</p>
          </li>
          <li id="uid101">
            <p noindent="true">Master : numerical analysis project, 30 H équivalent TD, M1, Polytech Nice Sophia.</p>
          </li>
        </sanspuceslist>
      </subsection>
      <subsection id="uid102" level="2">
        <bodyTitle>Supervision</bodyTitle>
        <sanspuceslist>
          <li id="uid103">
            <p noindent="true">PhD: Zheng Chen, L<formula type="inline"><math xmlns="http://www.w3.org/1998/Math/MathML" overflow="scroll"><msup><mrow/><mn>1</mn></msup></math></formula>-minimization in space mechanics, Univ. Paris
Saclay, defended September, 2016, J.-B. Caillau (co-supervised with Y. Chitour)
<ref xlink:href="#mctao-2016-bid67" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/></p>
          </li>
          <li id="uid104">
            <p noindent="true">PhD: Jérémy Rouot, , Univ. Nice Sophia Antipolis, Geometric and numerical methods in optimal control and application to orbit transfer and swimming at low Reynolds number.
Defended November, 2016, co-supervised by B. Bonnard and J.-B. Pomet. <ref xlink:href="#mctao-2016-bid47" location="biblio" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest"/></p>
          </li>
          <li id="uid105">
            <p noindent="true">PhD in progress: Achille Sassi, to be defended 01/2017, Numerical methods for
hybrid control and chance-constrained optimization problems, Univ. Paris
Saclay, J.-B. Caillau (co-supervised with M. Cerf, E. Trélat and H. Zidani)</p>
          </li>
          <li id="uid106">
            <p noindent="true">PhD in progress: Michaël Orieux, started 10/2015, Dynamical systems
and optimal control, Univ. Paris Dauphine,
J.-B. Caillau (co-supervised with J. Féjoz)</p>
          </li>
          <li id="uid107">
            <p noindent="true">PhD in progress: Zeinab Badreddine, started 09/2014, Sub-Riemannian Geometry and Optimal Transport,
co-supervised by L. Rifford and B. Bonnard.</p>
          </li>
          <li id="uid108">
            <p noindent="true">PhD in progress: Sébastien Fueyo, started 09/2016, Testing stability of nonlinear amplifier by frequency-domain methods.
J.-B. Pomet (co-supervised with L. Baratchart).</p>
          </li>
          <li id="uid109">
            <p noindent="true">PhD in progress: Alice Nolot, started 09/2016,
Sub-Riemannian geometry and optimal swimming at low Reynolds number.
B. Bonnard.</p>
          </li>
        </sanspuceslist>
      </subsection>
      <subsection id="uid110" level="2">
        <bodyTitle>Juries</bodyTitle>
        <p>In 2016, J.-B. Caillau referee for Jiamin Zhu (Univ. Paris 6) and Maxime
Chupin (Univ. Paris 6) PhD theses, for the HDR of Aude Rondepierre (Univ. Toulouse),
and jury member for the PhD thesis of
Clément Royer (Univ. Toulouse).</p>
      </subsection>
    </subsection>
    <subsection id="uid111" level="1">
      <bodyTitle>Popularization</bodyTitle>
      <p>Conference for high school students, "Ne votez pas, jugez !" (J.-B. Caillau),
<ref xlink:href="http://www.education.gouv.fr/cid59384/la-semaine-des-mathematiques.html" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">semaine
des maths 2016</ref>, Lycée Charles de Gaulle (Dijon) and
<ref xlink:href="https://project.inria.fr/mastic/conferences/algorithmes-jeux-graphes" location="extern" xlink:type="simple" xlink:show="replace" xlink:actuate="onRequest">MASTIC</ref>
initiative (Inria Sophia Antipolis).</p>
    </subsection>
  </diffusion>
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            <foreName>Jean-Baptiste</foreName>
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            <initial>J.-B.</initial>
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          <persName>
            <foreName>Thomas</foreName>
            <surname>Haberkorn</surname>
            <initial>T.</initial>
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            <foreName>Gabriel</foreName>
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            <foreName>Christoph</foreName>
            <surname>Schnörr</surname>
            <initial>C.</initial>
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        <imprint>
          <biblScope type="number">18</biblScope>
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            <orgName>de Gruyter</orgName>
          </publisher>
          <dateStruct>
            <month>December</month>
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          </dateStruct>
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    </biblStruct>
    
    <biblStruct id="mctao-2016-bid65" type="book" rend="year" n="cite:bonnard:hal-01405169">
      <identifiant type="doi" value="10.1007/978-3-319-27464-5"/>
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            <initial>B.</initial>
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            <foreName>Monique</foreName>
            <surname>Chyba</surname>
            <initial>M.</initial>
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        <imprint>
          <biblScope type="number">23</biblScope>
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            <orgName>Springer</orgName>
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            <foreName>Jérémy</foreName>
            <surname>Rouot</surname>
            <initial>J.</initial>
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            <foreName>Ludovic</foreName>
            <surname>Rifford</surname>
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