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This thesis considers the problem of robust geometric regulation for tracking and disturbance rejection of systems governed by delay differential equations. It is well known that geometric regulation can be highly sensitive to system parameters and hence such designs are not always robust. In particular, when employing numerical approximations to delay systems, the resulting finite dimensional models inherit natural approximation errors that can impact robustness. This demonstrates this lack of robustness and then addresses robustness by employing versions of robust regulation that have been developed for infinite dimensional systems. Numerical examples are given to illustrate the ideas and to test the robustness of the regulator. / M.S. / Recent years have seen a surge in the everyday application of complex mechanical and electrical systems. These systems can perform complex tasks; however, the increased complexity makes it harder to control them. An example of such a system is a semi-autonomous car designed to stay within a designated lane. One of the most commonly used approaches for controlling such systems is called output regulation. In the above example, the output regulator regulates the output of the car (position of the car) to follow the reference output (the road lane). Traditionally, the design of output regulators assumes complete knowledge of the system. However, it is impossible to derive equations that govern complex systems like a car. This thesis analyzes the robustness of output regulators in the presence of errors in the system. In particular, the focus is on analyzing output regulators implemented to delay-differential equations. These are differential equations where the rate of change of states at the current time depends on the states at previous times. Furthermore, this thesis addresses this problem by employing the robust versions of the output regulators.

The Equipment Controls and Electronics section (EN-STI-ECE) at CERN is developing a high precision piezo-actuated rotational stage for the UA9 crystal collimation project. This collaboration is investigating how tiny bent crystals can help to steer particle beams used in modern hadron colliders such as the Large Hadron Collider (LHC). Particles are deflected by following the crystal planar channels, "channeling" through the crystal. For high energy particles the angular acceptance for channeling is very low, demanding for a high angular precision mechanism, i.e. the rotational stage. Several control-related issues arising from the complexity and operational environment of the system make it difficult to design a controller that achieves the desired performance. This thesis investigates different control approaches that could be used to improve the tracking capability of the rotational stage. It shows that the IRC method could be used to efficiently control the rotational stage. Moreover it shows that a harmonic cancellation method could be used to increase the tracking accuracy by canceling known harmonic disturbances. The harmonic cancellation method (the RFDC) was implemented in this thesis and proposed as an add-on to the present control algorithm.

We present new adaptive control algorithms that address the problem of rejecting sinusoids with known frequencies that act on an unknown asymptotically stable linear time-invariant system. To achieve asymptotic disturbance rejection, adaptive control algorithms of this dissertation rely on limited or no system model information. These algorithms are developed in discrete time, meaning that the control computations use sampled-data measurements. We demonstrate the effectiveness of algorithms via analysis, numerical simulations, and experimental testings. We also present extensions to these algorithms that address systems with decentralized control architecture and systems subject to disturbances with unknown frequencies.

Shape memory alloys (SMAs) are metallic materials, which have two main stable crystalline phases: austenite, a high temperature phase and martensite, a low temperature phase. Austenite and martensite each have unique physical and mechanical properties, and transformation between these phases enables two effects known as the shape memory effect (SME) and superelasticity. When a material that displays the SME is plastically deformed at low temperature, a heat input will cause the SMA to return to its original shape before the deformation. At higher temperatures, the material displays an effect called superelasticity, where strains of up to 10% are recoverable. These characteristics of SMA allow for significant amounts of strain recovery, and enable the design of SMA actuators. The temperature in an SMA actuator is generally controlled by resistive heating, also know as joule heating, and the strain recovery capabilities are used to do work on a load, thereby creating an electro-mechanical actuator. SMA actuators have attractive properties such as high energy density, smooth and silent actuation, reduced part counts compared to traditional alternatives, and scalability down to the micromechanical level. The phase transformation in SMA actuators, however, is highly non-linear. Therefore, the use of SMA as actuators, for example in positioning systems, benefits from the development of good models to predict and control the materials. The goals of this work are to develop a model suitable for real-time implementation, and that reproduces the observed behaviour of SMA actuators. The model is then inverted and used to develop a model-based controller, used in conjunction with traditional PID control to improve the precision and robustness of SMA actuators. The modelling portion of this work consists of the development of a phenomenological SMA model. The forward model is split into three blocks: a heating block, a phase kinetics block and a mechanical block. Since joule heating is commonly used in SMA actuators to bring about an increase in temperature, the heating block presents equations to convert a current input into the temperature of the wire. The phase kinetics block equations convert the calculated temperature and applied stress to the fraction of martensite present in the SMA. Finally, the mechanical model calculates the strain in the material from the martensite fraction and the applied stress. Once the model equations are presented, experimental verification tests are shown to compare physical SMA behaviour with that predicted by the model. Each of the blocks of the forward model are then inverted in order to be used as a feedforward linearizing controller. The control section of this thesis deals with the response of two common types of SMA actuators: a constant force SMA actuator and a spring-biased SMA actuator. The response of the system to step and sinusoidal signals with period of 5 seconds is investigated using two types of controllers: a traditional PI controller and the inverse-model controller in feedforward with a PI controller in feedback. Additionally, the robustness of the system is investigated through the response of the system to transient and sinusoidal stress disturbances. The disturbance rejection is investigated on a constant force actuator both with and without the presence of a force sensor.

Shape memory alloys (SMAs) are metallic materials, which have two main stable crystalline phases: austenite, a high temperature phase and martensite, a low temperature phase. Austenite and martensite each have unique physical and mechanical properties, and transformation between these phases enables two effects known as the shape memory effect (SME) and superelasticity. When a material that displays the SME is plastically deformed at low temperature, a heat input will cause the SMA to return to its original shape before the deformation. At higher temperatures, the material displays an effect called superelasticity, where strains of up to 10% are recoverable. These characteristics of SMA allow for significant amounts of strain recovery, and enable the design of SMA actuators. The temperature in an SMA actuator is generally controlled by resistive heating, also know as joule heating, and the strain recovery capabilities are used to do work on a load, thereby creating an electro-mechanical actuator. SMA actuators have attractive properties such as high energy density, smooth and silent actuation, reduced part counts compared to traditional alternatives, and scalability down to the micromechanical level. The phase transformation in SMA actuators, however, is highly non-linear. Therefore, the use of SMA as actuators, for example in positioning systems, benefits from the development of good models to predict and control the materials. The goals of this work are to develop a model suitable for real-time implementation, and that reproduces the observed behaviour of SMA actuators. The model is then inverted and used to develop a model-based controller, used in conjunction with traditional PID control to improve the precision and robustness of SMA actuators. The modelling portion of this work consists of the development of a phenomenological SMA model. The forward model is split into three blocks: a heating block, a phase kinetics block and a mechanical block. Since joule heating is commonly used in SMA actuators to bring about an increase in temperature, the heating block presents equations to convert a current input into the temperature of the wire. The phase kinetics block equations convert the calculated temperature and applied stress to the fraction of martensite present in the SMA. Finally, the mechanical model calculates the strain in the material from the martensite fraction and the applied stress. Once the model equations are presented, experimental verification tests are shown to compare physical SMA behaviour with that predicted by the model. Each of the blocks of the forward model are then inverted in order to be used as a feedforward linearizing controller. The control section of this thesis deals with the response of two common types of SMA actuators: a constant force SMA actuator and a spring-biased SMA actuator. The response of the system to step and sinusoidal signals with period of 5 seconds is investigated using two types of controllers: a traditional PI controller and the inverse-model controller in feedforward with a PI controller in feedback. Additionally, the robustness of the system is investigated through the response of the system to transient and sinusoidal stress disturbances. The disturbance rejection is investigated on a constant force actuator both with and without the presence of a force sensor.

La manipulation aérienne a été un domaine de recherche actif ces dernières années, principalement parce que les applications actives des véhicules aériens autonomes (UAV en anglais), augmente l'employabilité de ces véhicules pour diverses applications.Le développement récent de la manipulation aérienne a trouvé des applications potentielles dans les deux domaines, militaires et civils. Les applications militaires incluent le patrouilleur des frontières, la détection des mines, la reconnaissance, etc., tandis que les applications civiles sont en matière de gestion des catastrophes, d'inspection des ponts, de construction, de livraison de matériel, de recherche et de sauvetage, etc.La recherche sur la robotique aérienne implique principalement des hélicoptères et des architectures de décollage et d'atterrissage verticales (VTOL). Le principal avantage de ces plates-formes est leur maniabilité et la capacité d'effectuer des vols stationnaires, ce qui est essentiel pour les applications. Cette thèse porte sur les avions VTOL, où l'hélicoptère à quatre rotors ou quadrirotor est principalement étudié.En ce qui concerne le problème de la manipulation aérienne, la quantité d'applications augmente, mais en même temps, la complexité de la modélisation et du contrôle d'un tel système est également plus grande. L'un des plus grands défis réside dans leur charge utile limitée. Certaines approches ont essayé de résoudre le problème en utilisant plusieurs robots pour transporter des charges utiles avec des pinces ou des câbles, où leurs effecteurs et pinces doivent être légers eux-mêmes et capables de saisir des formes complexes. Un autre défi est que la dynamique du robot est considérablement modifiée par l'ajout de charges utiles. Cependant, pour le transport de la charge utile, il est nécessaire que les robots puissent estimer l'inertie de la charge utile et s'y adapter pour améliorer les performances de suivi.Selon les antécédents et les défis sur les véhicules VTOL portant des charges utiles ou des manipulateurs, la contribution du présent travail est centrée sur la modélisation et la conception d'une loi de commande non linéaire et une analyse de stabilité formelle pour la stabilisation asymptotique d'un véhicule VTOL portant un bras manipulateur. Pour cela, un modèle général d'un quadrirotor portant un bras manipulateur est proposé. Après cela, une loi de commande presque globalement asymptotique lisse pour la stabilisation de l'attitude qui prend en compte les effets de mouvement du bras est conçue. Une fois que le problème d'attitude est résolu, il est possible de concevoir un contrôleur non linéaire globalement asymptotique pour la dynamique de position basée sur l'utilisation de somme des fonctions saturés afin de prendre en compte les limitations des actionneurs. Enfin, certaines expériences pour valider les lois de commande proposées sont effectuées. / Aerial manipulation has been an active area of research in recent years, mainly because the active tasking of Unmanned Aerial Vehicles (UAV) increases the employability of these vehicles for various applications.The recent development of the aerial manipulation has found potential applications in both, military and civilian domains. Military applications include border patrolling, mine detection, reconnaissance, etc., while civilian applications are in disaster management, bridge inspection, construction, material delivery, search and rescue, etc.The research on aerial robotics has mainly involved helicopters and Vertical Take-off and Landing (VTOL) architectures. The main advantage of these platforms is theirmaneuverability and the capacity to perform hovers, which is essential for the applications. This thesis deals with VTOL aircrafts, where the four rotor helicopter, quadcopter or quadrotor is mainly studied.Regarding the problem of aerial manipulation, the amount of applications are increased, but at the same time the complexity of modeling and control of such a system are equally bigger. One of the biggest challenges arise from their limited payload. Some approaches have tried to solve the problem using multiple robots to carry payloads with grippers or with cables, where their end effectors and grippers have to be lightweight themselves and capable of grasping complex shapes. Another challenge is that the dynamics of the robot are significantly altered by the addition of payloads. However, for payload transport, it is necessary that the robots are able to estimate the inertia of the payload and adapt to it to improve tracking performance.According to the background and challenges on VTOL vehicles carrying payloads or manipulators, the contribution of the present work is centered on the modelling and the design of a nonlinear control and a formal stability analysis for the asymptotical stabilization of a VTOL vehicle carrying a manipulator arm. For this a general model of a quadcopter carrying a manipulator arm is proposed. After that, a smooth almost globally asymptotically control law for attitude stabilization which takes into account the arm motion effects is designed. Once the attitude problem is solved, it is possible to design a a globally asymptotically nonlinear controller for the translational dynamics based in the usage of nested and sum of saturation functions in order to take into account the actuators limitations. Finally, some experiments in order to validate the proposed control laws are carried out.

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