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Traitement de l'Information et Systèmes
Département Commande des Systèmes et Dynamique du vol


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Publications, papers published in December 1999/communications publiées en décembre 1999

Bibliography

1
J.-P. Chrétien.
Optimal filtering of wind and temperature balloon sounding.
In CNES, editor, Launch Vehicles Vibrations Proceedings, pages 233-242, Toulouse (France), 14 - 16 December 1999. CNES.
The determination of extreme wind-shear conditions during the atmospheric phase of the trajectory of a launcher is a critical point as it is used to specify extremal loads on the launcher itself and on its payload. Atmospheric models used to predict extremal shears rely on parameters which must ne numerically known with a sufficient precision : the in situ simultaneous measurement of the horizontal wind velocity (two components) and the atmospheric temperature, using an instrumented balloon, is one of the ways offered. In spite of the fact that the in situ measurement is non stationary, spectral analysis has been shown to be an efficient tool to separate different contributions to the measurement. In a normalized spectral diagram (power spectral density as a function of spatial frequency), 3 zones can be recognized:
  • in low frequency (over a spatial resolution of 100 m), a meso-scale stochastic atmospheric model, characterized by a linear decrease of the spectrum, following a slope around -3 (``spectral index''),
  • in mean frequency, a dominant effect of the balloon dynamics, excited by a source of noise independent of the meso-scale model,
  • in high frequency (up to the Nyquist spatial frequency). a dominant effect of the location device noise, particularly in the case of radar location of the balloon ; use of the Global Positioning System (GPS) reduces significantly this source of error, which lies anyway in a frequency range in which the meso-scale atmospheric model is no more valid
The main filtering problem to improve the wind velocity profiles as a function of altitude is then to extract the correct atmospheric model in the frequency range of interest (from 100 m to 1000 m resolution) in spite of the overlap of the spurious balloon motions in this frequency range. The temperature profiles require less filtering in this frequency range as they are less depending upon the balloon motions. The paper is dedicated to the application of optimal filtering to this problem : visualizing the atmospheric model as a reference signal and balloon motion as a measurement noise lead naturally to apply Wiener theory, in the simplified case where the signal and noise are uncorrelated. The filter minimizing the estimation error in the root mean square sense is simply obtained in frequency domain by dividing the reference model spectrum by the measurement spectrum. This can be done in two ways :
  • pointwise in frequency, using the estimated measurement spectrum,
  • analytically, using representations of both signal and noise as functions of the operational variable z (as the data are sampled by the location and wind measurement .
In order to be able to apply analytically the theory, we consider first the possible analytical models for the noise (combining balloon dynamics and measurement device). A second section is devoted to the synthesis of optimal filters in the simplest canonical case of a second order atmospheric spectrum (Wiener-Levy process for the signal) and a discrete white noise for the balloon. The data being processed a posteriori, a non causal filter can be used, which theoretical performances are calculated and verified by statistics on a set of realizations. The robustness to mismatch in signal or noise model is also discussed. It is thus shown that optimal filtering extracts the meso-scale model in spite of spurious motions of the balloon in the frequency range of interest, and that is is possible to deal with more complicated balloon models (pendular motion for example). In the frame of the canonical model, a comparison is then.

2
H. D. Tuan and P. Apkarian.
Low nonconvex rank bilinear matrix inequalities: Algorithms and applications.
In CDC 1999 - 38th IEEE Conference on Decision and Control, Phoenix (USA), 8 - 11 December 1999. IEEE.
A new Branch and Bound (BB) algorithm for solving a general class of Bilinear Matrix Inequality (BMI) problem is proposed. First, Linear Matrix Inequality (LMI) constraints are incorporated into BMI constraints in a special way to take advantage of useful informations on nonconvex terms. Then, the nonconvexity of BMI is centralized in coupling constraints so that when the latter are omitted, we get a relaxed LMI problem for computing lower bounds. As in our previous developments, the branching is performed in a reduced dimensional space of complicating variables. This makes the approach practical even with a large dimension of overall variables. Applications of the algorithm to several test problems of robust control are discussed.

3
P. Apkarian, H. Kajiwara, and P. Gahinet.
LPV techniques for control of an inverted pendulum.
IEEE Control System Magazine, 1999.
The purpose of the paper is to demonstrate the ability of LPV (Linear Parameter Varying) control techniques to handle difficult nonlinear control problems. The focus in this paper is on the wide range stabilization of an arm-driven inverted pendulum. Two different LPV control techniques are used to design nonlinear controllers that achieve stabilization of the pendulum over the maximum range of operating conditions while providing time- and frequency-domain performances. The merits of each of these techniques are investigated and the improvements over more classical LTI (Linear Time-Invariant) control schemes such as Hinfinite or controllers are discussed. A particular emphasis is put on the real-time implementation of these controllers for the inverted pendulum experiment. It is shown in the application that suitable multi-objective extensions of the standard characterization of LPV controllers allow us to cope with sampling rate implementation constraints. Finally, a complete validation of the proposed LPV controller structures is carried out through a set of realistic nonlinear simulations but also by means of physical experiment records.

4
C. Cossart and C. Tessier.
Filtre de kalman et processus de révision et de mise jour : une étude comparée.
Revue d'Intelligence Artificielle, 1999.
Partant du constat qu'il existe des similitudes dans les objectifs de l'estimation numérique et de la révision et de la mise à jour, nous proposons d'effectuer un rapprochement et une comparaison des différents processus. Nous étudions ainsi en détail les points communs et différences de l'estimation numérique d'une part - à travers le filtre de Kalman mono et multimodèle - et des mécanismes de révision et de mise à jour d'autre part - depuis les postulats d'AGM à la mise à jour généralisée de Boutilier. Nous soulignons l'évolution progressive des processus de changement de croyances vers les principes du filtrage de Kalman et identifions les ingrédients d'un estimateur symbolique dans le cas particulier du suivi de situation.

5
M. Chilali, P. Gahinet, and P. Apkarian.
Robust pole placement in LMI regions.
IEEE TAC, 44(12):2257-2270, December 1999.
This paper discusses analysis and synthesis techniques for robust pole placement in LMI regions, a class of convex regions of the complex plane that embraces most practically useful stability regions. The focus is on linear systems with static uncertainty on the state matrix. For this class of uncertain systems, the notion of quadratic stability and the related robustness analysis tests are generalized to arbitrary LMI regions. The resulting tests for robust pole clustering are all numerically tractable since they involve solving linear matrix inequalities (LMIs), and cover both unstructured and parameter uncertainty. These analysis results are then applied to the synthesis of dynamic output-feedback controllers that robustly assign the closed-loop poles in a prescribed LMI region. With some conservatism, this problem is again tractable via LMI optimization. In addition, robust pole placement can be combined with other control objectives such as H_2 or Hinf performance to capture realistic sets of design specifications. Physically-motivated examples demonstrate the effectiveness of this robust pole clustering technique.

6
P. Coton, J. C. Monnier, R. Stuff, L. Dieterle, and G. Schneider.
Characterization of the wake far field from high lift configurations of the airbus A300 by PIV measurements in the onera lille flight analysis laboratory.
Aerospace Science and Technology, 1999.
Une nouvelle méthodologie a récemment été développée pour l'étude du sillage des avions. Les essais se déroulent dans le Laboratoire d'Analyse du Vol de l'ONERA/Lille. Une maquette d'Airbus A 300 au 22ème est catapultée puis évolue dans un espace d'observation de 30 m de long, 9 m de large et 10 m de haut. Tra-jectoire et attitude de la maquette sont déterminées au moyen d'une instrumenta-tion embarquée et de mesures faites au sol. L'écoulement est visualisé par de la fumée et mesuré par PIV (Vélocimétrie par Images de Particules) dans un réfé-rentiel fixe par rapport au sol. Ces mesures ont été effectuées en partie dans le cadre du programme de coopération ONERA/DLR et en partie dans le cadre du projet européen de recherche WAVENC (Wake Vortex Evolution in Far-Wake Region and Wake Vortex Encounter). Deux configurations hyper-sustentées, sans nacelles, ont été testées. Dans la première configuration seuls les volets.

7
H. D. Tuan, P. Apkarian, and M. James.
Parameterized linear matrix inequalities for nonlinear discrete H_infty control.
In CDC 1999 - 38th IEEE Conference on Decision and Control, Phoenix (USA), 8 - 11 December 1999. IEEE.
A new approach based on parameterized linear matrix inequalities (PLMIs) for solving nonlinear discrete $\clH_{\infty}$ control is proposed. The ``curse of dimensionality'' is one of the main obstacles preventing nonlinear $H_\infty$ control theory to be used in practice. However, in most applications, nonlinearity of a nonlinear system is caused by a few variables with dimension much lower than the plant dimension. Considering such nonlinear variables as parameters, the system can be handled as a family of linear systems depending on parameters in a reduced-dimension space. Then, PLMI tools can be used to render the nonlinear $\clH_{\infty}$ control problem computationally tractable. Moreover, this approach can work well for output feedback problem giving a finitely dimensional control instead of a customized infinitely dimensional one.

8
C. Cossart.
Un estimateur symbolique pour le suivi de situation.
Thèse de doctorat Sup'Aéro, (20), décembre 1999.
Le thème des travaux est l'élaboration et le suivi de situation dans un monde dynamique pouvant évoluer librement, dans le cadre de missions de surveillance, de reconnaissance ou de renseignement. Le problème central de la reconnaissance de situations est la mise en correspondance des données visuelles avec des modèles d'actions et d'enchaînements temporels d'actions, définis a priori et censés décrire au mieux les situations susceptibles d'être observées dans l'environnement considéré. Il est renforcé par un problème de rigidité des modèles et de l'algorithme de mise en correspondance. Dans ce contexte, l'objectif de la thèse est de proposer un système d'élaboration et de suivi de situation, au niveau symbolique, capable de prendre en compte, d'une part, les imperfections de données et, d'autre part, les écarts existant entre les comportements réels et les comportements prédéfinis dans les modèles. La construction d'un tel système, désigné sous le nom d'estimateur symbolique, a été réalisée en deux étapes : spécification et formalisation. Un premier ensemble de spécifications a été déduit de l'étude du système conçu dans le cadre du projet Perception et d'approches récentes de la reconnaissance d'actions. Des spécifications plus précises ont été déduites de la confrontation du filtre de Kalman et des processus de révision et de mise à jour d'ensembles de croyances, les deux types de démarches présentant des points communs avec le problème du suivi de situation. L'estimateur symbolique construit en réponse aux spécifications est un processus en deux étapes, prédiction et recalage, qui autorise des mises en correspondance données-modèles imparfaites. Il manipule des relations de préférence qualitatives, qui représentent l'incertitude sur la situation en cours dans l'environnement. Le principe de l'estimateur ainsi défini est appliqué à la surveillance d'un parking. This thesis deals with automatic scene recognition in dynamic environments, for surveillance and intelligent systems, autonomous vehicles or decision aid systems. The recognition process is based on the matching of visual data with action prototypes and temporal plan prototypes. Such a process is characterized by uncertainty issues linked both to the models and to the matching algorithm: on the one hand, data may be uncertain and, on the other hand, the matching quality depends on the accuracy and the relevance of the models. In such a context, our work aims at designing a symbolic estimation tool, in which imperfect data are taken into account and imperfect matchings are allowed. The design of such an estimator is achieved through two steps: specification and formalization. In order to deduce specifications, the situation assessment system designed in the framework of Perception project is analysed and recent approaches of action recognition are studied. More precise specifications are deduced from a confrontation of Kalman filtering and belief revision and update processes as both types of processes have common characteristics with situation assessment problem. The symbolic estimation tool for situation assessment is a two-step process, prediction and correction, in which imperfect matchings are defined. It handles qualitative preference relations that encode the uncertainty on the situation in progress in the observed environment. The principle of the symbolic estimator is illustrated on the surveillance of a parking-lot.

9
H. D. Tuan, P. Apkarian, and H. Tuy.
Advanced global optimization algorithms for parameterized LMIs.
In CDC 199 - 38th IEEE Conference on Decision and Control, Phoenix - Arizona (USA), 7 - 10 December 1999. CDC.
A new approach based on parameterized linear matrix inequalities (PLMIs) for solving nonlinear discrete Hinfinity control is proposed. The ``curse of dimensionality'' is one of the main obstacles preventing nonlinear Hinfinity control theory to be used in practice. However, in most applications, nonlinearity of a nonlinear system is caused by a few variables with dimension much lower than the plant dimension. Considering such nonlinear variables as parameters, the system can be handled as a family of linear systems depending on parameters in a reduced-dimension space. Then, PLMI tools can be used to render the nonlinear Hinfinity control problem problem computationally tractable. Moreover, this approach can work well for output feedback problem giving a finitely dimensional control instead of a customized infinitely dimensional one.

10
Y. Meiller and P. Fabiani.
Perception-action dilemma at planning time : Getting the best out of game theory and classical planning.
In 18th Workshop of the UK Planning and Scheduling Special Interest Group, Salford (UK), 15 - 16 December 1999. University of Salford.
Dealing with uncertainty in motion planning combines a number of problems of estimation, planning and execution control. Classical methods in Planning can take advantage of the structure of the workspace, but handling uncertainty within these frameworks generally raises a question of representation compatibility. Game theory offers efficient tools for decision making in the presence of uncertainty, but often leads to a combinatorial exploration of the decision tree. The association of both frameworks seems to be a promising approach in order to combine symbolic reasoning tools with representations of numerical uncertainty coming from sensory information. We propose to introduce Graphplan-like techniques in game-theoretic planning. Colored Petri nets allow us to present both standard forward state space search and Graphplan like approaches within the same formalism. Expected benefits of this proposal are discussed together with the example of a possible application to the perception-action dilemma.

11
L. Chaudron and N. Maille.
The continuous inference model based on the analysis of mathematical reasoning.
AI Communications, The European Journal on Artificial Intelligence, 1999.
In this paper, we aim at designing a flexible model for the reasoning of cooperating inferential agents.The context is mathematical problem solving and the model is based on an experimental analysis of oral tests. Our contribution consists in: i) the analysis of real cases and the induction of empirical laws, ii) the definition of a general model, called "continuous inference", dedicated to problem representation, iii) the logical and algebraic description of the model thanks to the cube lattice structure (and its implementation).

12
L. Chaudron and N. Maille.
Le modèle des cubes : représentation algébrique des conjonctions de propriétés.
Revue d'Intelligence Artificielle, 1999.
Dans cet article, nous présentons un modèle, dit des « Cubes », destiné à formaliser tout type de connaissance qui soit fondée sur des conjonctions de propriétés. Ce modèle est utile pour toute approche dans laquelle il est nécessaire de mathématiser fidèlement la connaissance ainsi que les moyens intrinsèques d'en comparer les éléments : modélisation de la connaissance de perception, représentation d'activités, fusion symbolique, etc.

13
J.-L. Farges.
Neural networks and dynamic programming for robust landing.
International JournalEngineering Applications of Artificial Intelligence, 1999.
This paper deals with the optimization of non linear state feedback for systems submitted to bounded perturbations and assessed through the value of the final state of their trajectory. Neural Networks are used to approximate either the optimal cost to go or the optimal control and the worst perturbation during the search of the solution of minimum of maximum by Dynamic Programming. In function of the quantity approximated, two kind of algorithms are proposed. The methods are applied to a landing problem in presence of unknown but bounded wind. For this problem, we show that the initialization of the Neural Networks approximating the functions can be performed through the approximation of elementary logical functions. The study and the associated numerical experiments indicate that it seems more adequate to approximate only the value function. Nevertheless, in this context, some problems remain open at the level of the convergence of the on-line retropropagation and the adaptation of only some given network weights may induce improvements.


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