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Direct Adaptive Control Synthesis for Uncertain Nonlinear SystemsFu, Hsu-sheng 22 February 2009 (has links)
The dissertation addresses direct adaptive control frameworks for Lyapunov stabilization of the MIMO nonlinear uncertain systems for both uncertain
discrete-time and continuous-time systems. For system theory, the development of continuous-time theory always comes along with its discrete-time counterpart. However, for direct adaptive control frameworks we find relative few Lyapunov-based results published, which is mainly due to difficulty to find feasible Lyapunov candidates and to prove negative definiteness of the Lyapunov difference.
Furthermore, digital computer is widely used in
all fields. Most of time, we have to deal with the direct source of discrete-time signals, even the discrete-time signals arise from continuous-time settings as results of measurement or data collection process. These motivate our study in this field.
For discrete-time systems, we have investigated the results with trajectory dependent hypothesis, where the Lyapunov candidate function V combines the information from the current state k and one step ahead k-1 along the track x(k), for k≥0. The proposed frameworks guarantee partial stability
of the closed-loop systems, such that the feedback gains stabilize the closed-loop system without the knowledge of the system parameters. In addition,
our results show that the adaptive feedback laws can be characterized by Kronecker calculus.
Later, we release this trajectory dependent hypothesis
for normal discrete-time nonlinear systems. At the same time, the continuous-time cases are also studied when system with matched disturbances, where the disturbances can be characterized by
known continuous function matrix and unknown parameters. Here, the trajectory dependent Lyapunov candidates (tdLC), so long as the time step
|t(k)-t(k-1) | ≤ £_ and the corresponding track |x(k)-x(k-1)| ≤ £` are sufficiently small, only exist in discrete-time case. In addition, we have extended the above control designs to systems with exogenous disturbances and
£d2 disturbances. Finally, we develop a robust direct adaptive control framework for linear uncertain
MIMO systems under the variance of unknow system matrix from given stable solution is bounded, that is |A-Ac| ¡Ý |B Kg| ≤ |£GA|.
In general, through Lyapunov-based design we can obtain the global solutions and direct adaptive control design can simultaneously achieve parameter estimation and closed-loop stability.
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Contrôle adaptatif robuste. Application au contrôle d'attitude de satellites / Robust adaptive control. Application to satellite attitude controlLeduc, Harmonie 22 September 2017 (has links)
Cette thèse porte sur la commande adaptative directe robuste et son application au contrôle d’attitude des satellites de la filière Myriade du CNES. Après avoir présenté les différents types de commande variant dans le temps, nous rappelons les caractéristiques d’un contrôleur adaptatif direct, en particulier le fait que la seule connaissance d’un retour de sortie stabilisant le système à contrôler suffit pour concevoir un contrôleur adaptatif direct. Parallèlement, nous présentons la théorie des systèmes descripteurs. Modéliser un système sous forme descripteur est non conventionnel mais présente de nombreux avantages dans le contexte de la commande adaptative directe robuste. A l’aide des résultats existants sur la commande adaptative directe d’une part, et de la théorie des systèmes descripteurs d’autre part, nous fournissons une méthode permettant de calculer, connaissant un retour de sortie constant, les paramètres d’un contrôleur adaptatif direct robuste stabilisant. Cette méthode repose sur la résolution d’inégalités matricielles linéaires. Le contrôleur adpatatif est plus robuste que le contrôleur constant, mais on ne peut prouver que la stabilité globale que vers un voisinage du point d’équilibre. Nous présentons ensuite une méthode, également basée sur la résolution d’inégalités matricielles linéaires, permettant de concevoir un contrôleur adaptatif direct robuste de meilleur niveau de rejet des perturbations extérieures que le contrôleur constant à partir duquel il est construit. L’ensemble de ces résultats théoriques est ensuite appliqué au contrôle d’attitude des satellites de la filière Myriade du CNES. En particulier, nous concevons un contrôleur d’attitude stabilisant le satellite quelle que soit la valeur de son inertie. Ce contrôleur d’attitude est également capable d’éviter aux roues à réaction du satellite de saturer. Nous concevons ensuite un contrôleur d’attitude adaptatif, robuste, et qui rejette mieux les perturbations extérieures que le contrôleur constant à partir duquel il est construit. Ce contrôleur constant est d’ailleurs actuellement implémenté à bord des satellites de la filière Myriade du CNES. Enfin, nous validons l’ensemble des résultats de cette thèse à l’aide d’un simulateur SCAO du CNES, où nous simulons le déploiement des mâts d’un satellite, ainsi que des scénarii de sauts de guidage. / This manuscript deals with robust direct adaptive control, and its application to CNES microsatellites attitude control. After listing the different types of time-varying controllers, we recall the characteristics of direct adaptive control. In particular, we recall that the knowledge of a stabilizing static output feedback is sufficient to design a direct adaptive controller. In parallel, we introduce the descriptor system theory. Modelizing a system into descriptor form is not usual but fits well with robust direct adaptive control. Starting from existing results about adaptive control and descriptor system theory, we provide an LMI based method which allows to compute, with the knowledge of a stabilizing static output feedback, the parameters of a stabilizing direct adaptive controller. A first result proves that the adaptive controller is at least as robust as the static output feedback. The second result allows to prove improved robustness at the expense of relaxing stability of the equilibrium point to practical stability, that is convergence to a neighborhood of the equilibrium. Then, we provide a method, LMI based as well, which allows to design a robust direct adaptive controller which has a better level of rejection of the perturbations than the static output feedback from which it is designed. All these theoretical results are applied to the attitude control of CNES microsatellites. We design a controller which stabilizes the attitude of the satellite whatever the value of its inertia. This attitude controller can also avoid the satellite reaction wheels to saturate. We design another robust adaptive attitude controller which has a better level of rejection of the perturbations than the static controller which is currently implemented aboard CNES satellites. Finally, we validate all the results of this manuscript by simulating on a AOCS CNES simulator the deployment of the satellite masts and some guiding jumps.
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