Modeling and Model-Based Control Of Multi-Mode Combustion Engines for Closed-Loop SI/HCCI Mode Transitions with Cam Switching Strategies.

Homogeneous charge compression ignition (HCCI) combustion has been investigated by many researchers as a way to improve gasoline engine fuel economy through highly dilute unthrottled operation while maintaining acceptable tailpipe emissions. A major concern for successful implementation of HCCI is that it's feasible operating region is limited to a subset of the full engine regime, which necessitates mode transitions between HCCI and traditional spark ignition (SI) combustion when the HCCI region is entered/exited. The goal of this dissertation is to develop a methodology for control-oriented modeling and model-based feedback control during such SI/HCCI mode transitions. The model-based feedback control approach is sought as an alternative to those in the SI/HCCI transition literature, which predominantly employ open-loop experimentally derived actuator sequences for generation of control input trajectories. A model-based feedback approach has advantages both for calibration simplicity and controller generality, in that open-loop sequences do not have to be tuned, and that use of nonlinear model-based calculations and online measurements allows the controller to inherently generalize across multiple operating points and compensate for case-by-case disturbances. In the dissertation, a low-order mean value modeling approach for multi-mode SI/HCCI combustion that is tractable for control design is described, and controllers for both the SI to HCCI (SI-HCCI) and HCCI to SI (HCCI-SI) transition are developed based on the modeling approach. The model is shown to fit a wide range of steady-state actuator sweep data containing conditions pertinent to SI/HCCI mode transitions, and is extended to capture transient SI-HCCI transition data through using an augmented residual gas temperature parameter. The mode transition controllers are experimentally shown to carry out SI-HCCI and HCCI-SI transitions in several operating conditions with minimal tuning, though the validation in the SI-HCCI direction is more extensive. The model-based control architecture is also equipped with an online parameter updating routine, to attenuate error in model-based calculations and improve robustness to engine aging and cylinder to cylinder variability. Experimental examples at multiple operating conditions illustrate the ability of the parameter update routine to improve controller performance by using transient data to tune the model parameters for enhanced accuracy during SI-HCCI mode transitions.PhDMechanical EngineeringUniversity of Michigan, Horace H. Rackham School of Graduate Studieshttp://deepblue.lib.umich.edu/bitstream/2027.42/113351/1/pgoz_1.pd

Soft-Landing Control of Short-Stroke Reluctance Actuators

Los actuadores de reluctancia se utilizan ampliamente debido a sus altas densidades de fuerza y baja disipación de calor. En particular, los actuadores de reluctancia simples de una sola bobina de carrera corta, como los relés electromecánicos y las electroválvulas, son la mejor opción para operaciones de conmutación de encendido y apagado en muchas aplicaciones debido a su bajo coste, tamaño y masa. Sin embargo, un inconveniente importante es el fuerte impacto al final de cada conmutación, que provoca rebotes, desgaste mecánico y ruido acústico. Son fenómenos muy indeseables que restan valor a las ventajas evidentes de estos actuadores y limitan su rango de aplicaciones potenciales.Esta tesis se centra en el desarrollo y estudio de soluciones de control de aterrizaje suave para actuadores de reluctancia de carrera corta, con el objetivo de minimizar sus velocidades de impacto. Es importante indicar que la eficiencia de dichos dispositivos se produce a costa de serios retos teóricos y prácticos en cuanto a su control, por ejemplo, dinámicas rápidas, híbridas y altamente no lineales, fenómenos electromagnéticos complejos, variabilidad entre unidades y falta de medidas de posición durante el movimiento.El punto de partida es la modelización del sistema, teniendo en cuenta sus subsistemas interconectados eléctricos, magnéticos y mecánicos. El objetivo principal de los modelos es servir para el desarrollo de métodos de control y estimación. Por lo tanto, se trata de modelos de parámetros concentrados expresados como representaciones del espacio de estados. Se especifican diferentes fenómenos electromagnéticos, con especial atención a la histéresis magnética. Se proponen dos tipos de modelos de diferente complejidad según se incorpore o se desprecie el fenómeno de la histéresis magnética.El primer enfoque para el control del aterrizaje suave es el diseño óptimo de las trayectorias de posición y sus correspondientes señales de entrada. La propuesta tiene en cuenta la incertidumbre en la posición del contacto y, por tanto, las soluciones obtenidas son más robustas. Mientras que las señales de entrada generadas son eficaces para las estrategias de control en lazo abierto, las trayectorias de posición generadas pueden utilizarse controles de prealimentación o de retroalimentación.Para mejorar la robustez de los controladores de lazo abierto, también proponemos una estrategia run-to-run que adapta iterativamente las señales de entrada. En concreto, está diseñada para trabajar conjuntamente con un controlador de prealimentación basado en las mencionadas trayectorias de posición construidas de forma óptima. Para el algoritmo de aprendizaje ciclo a ciclo, se elige una técnica de optimización, se ajusta y se compara con dos alternativas.Otro enfoque explorado es el control de retroalimentación para el seguimiento de trayectorias predefinidas de posición. La solución propuesta es un controlador estrictamente conmutativo en modo deslizante. Está enfocado en la simplicidad para facilitar su implementación, al tiempo que se tiene en cuenta la dinámica híbrida. Los análisis teóricos y simulados demuestran que el aterrizaje suave es posible con tasas de muestreo razonables.Los controladores de retroalimentación y otros controladores de seguimiento requieren mediciones o estimaciones precisas de la posición. Como la medición de la posición raramente es práctica, parte de la investigación se dedica al diseño de estimadores de estado. La principal propuesta es un suavizador Rauch-Tung-Striebel ampliado para sistemas no lineales, que incluye varias ideas nuevas relacionadas con el modelo discreto, las entradas y las salidas. Los análisis simulados demuestran que el efecto combinado de las nuevas adiciones da lugar a mucho mejores estimaciones de la posición.Reluctance actuators are widely used due to their high force densities and low heat dissipation. In particular, simple short-stroke single-coil reluctance actuators, such as electromechanical relays and solenoid valves, are the best choice for on-off switching operations in many applications because of their low cost, size and mass. However, a major drawback is the strong impact at the end of each commutation, which provokes bouncing, mechanical wear and acoustic noise. They are very undesirable phenomena that detract from the evident advantages of these actuators and limit their range of potential applications. This thesis focuses on the development and study of soft-landing control solutions for short-stroke reluctance actuators, aiming at minimizing their impact velocities. It is important to indicate that the efficiency of the aforementioned devices comes at the cost of serious theoretical and practical challenges regarding their control, e.g., fast, hybrid and highly nonlinear dynamics, complex electromagnetic phenomena, unit-to-unit variability and lack of position measurements during motion. The starting point is the system modeling, accounting for their interconnected electrical, magnetic and mechanical subsystems. The main purpose of the models is to be used for the development of control and estimation methods. Therefore, they are lumped-parameter models expressed as state-space representations. Different electromagnetic phenomena are specified, with special attention to the magnetic hysteresis. Two model types of different complexities are proposed depending on whether the magnetic hysteresis phenomenon is incorporated or neglected. The first approach for soft-landing control is the optimal design of position trajectories and their corresponding input signals. The proposal considers uncertainty in the contact position, and hence, the obtained solutions are more robust. While the generated input signals are effective for open-loop control strategies, the generated position trajectories can be used in feedforward or feedback control. In order to improve the robustness of open-loop controllers, we also propose a run-to-run strategy that iteratively adapts the input signals. Specifically, it is designed to work in conjunction with a feedforward controller based on the aforementioned optimally constructed position trajectories. For the cycle-to-cycle learning algorithm, an optimization technique is chosen, adjusted and compared to two alternatives. Another explored approach is feedback control for tracking predefined position trajectories. The proposed solution is a purely switching sliding-mode controller. The focus is on simplicity to facilitate its implementation, while also taking into account the hybrid dynamics. Theoretical and simulated analyses show that soft landing is achievable with reasonable sampling rates. Feedback and other tracking controllers require accurate measurements or position estimations. As measuring the position is rarely practical, part of the research is devoted to the design of state estimators. The main proposal is an extended Rauch–Tung–Striebel smoother, which includes several new ideas regarding the discrete model, the inputs and the outputs. Simulated analyses demonstrate that the combined effect of the novel additions results in much better position estimations.<br /

Research on Information Flow Topology for Connected Autonomous Vehicles

Information flow topology plays a crucial role in connected autonomous vehicles (CAVs). It describes how CAVs communicate and exchange information with each other. It predominantly affects the platoon\u27s performance, including the convergence time, robustness, stability, and scalability. It also dramatically affects the controller design of CAVs. Therefore, studying information flow topology is necessary to ensure the platoon\u27s stability and improve its performance. Advanced sliding mode controllers and optimisation strategies for information flow topology are investigated in this project. Firstly, the impact of information flow topology on the platoon is studied regarding tracking ability, fuel economy and driving comfort. A Pareto optimal information flow topology offline searching approach is proposed using a non-dominated sorting genetic algorithm (NSGA-II) to improve the platoon\u27s overall performance while ensuring stability. Secondly, the concept of asymmetric control is introduced in the topological matrix. For a linear CAVs model with time delay, a sliding mode controller is designed to target the platoon\u27s tracking performance. Moreover, the Lyapunov analysis is used via Riccati inequality to guarantee the platoon\u27s internal stability and input-to-output string stability. Then NSGA-II is used to find the homogeneous Pareto optimal asymmetric degree to improve the platoon\u27s performance. A similar approach is designed for a nonlinear CAVs model to find the Pareto heterogeneous asymmetric degree and improve the platoon\u27s performance. Thirdly, switching topology is studied to better deal with the platoon\u27s communication problems. A two-step switching topology framework is introduced. In the first step, an offline Pareto optimal topology search with imperfect communication scenarios is applied. The platoon\u27s performance is optimised using a multi-objective evolutionary algorithm based on decomposition (MOEA/D). In the second step, the optimal topology is switched and selected from among the previously obtained Pareto optimal topology candidates in real-time to minimise the control cost. For a continuous nonlinear heterogeneous platoon with actuator faults, a sliding mode controller with an adaptive mechanism is developed. Then, the Lyapunov approach is applied to the platoon\u27s tracking error dynamics, ensuring the systems uniformly ultimately bounded stability and string stability. For a discrete nonlinear heterogeneous platoon with packet loss, a discrete sliding mode controller with a double power reaching law is designed, and a modified MOEA/D with two opposing adaptive mechanisms is applied in the two-step framework. Simulations verify all the proposed controllers and frameworks, and experiments also test some. The results show the proposed strategy\u27s effectiveness and superiority in optimising the platoon\u27s performance with multiple objectives

Human-centered Electric Prosthetic (HELP) Hand

Through a partnership with Indian non-profit Bhagwan Mahaveer Viklang Sahayata Samiti, we designed a functional, robust, and and low cost electrically powered prosthetic hand that communicates with unilateral, transradial, urban Indian amputees through a biointerface. The device uses compliant tendon actuation, a small linear servo, and a wearable garment outfitted with flex sensors to produce a device that, once placed inside a prosthetic glove, is anthropomorphic in both look and feel. The prosthesis was developed such that future groups can design for manufacturing and distribution in India

Position Control of Pneumatic Actuator Using Self-Regulation Nonlinear PID

The enhancement of nonlinear PID (N-PID) controller for a pneumatic positioning system is proposed to improve the performance of this controller. This is executed by utilizing the characteristic of rate variation of the nonlinear gain that is readily available in N-PID controller. The proposed equation, namely, self-regulation nonlinear function (SNF), is used to reprocess the error signal with the purpose of generating the value of the rate variation, continuously. With the addition of this function, a new self-regulation nonlinear PID (SN-PID) controller is proposed. The proposed controller is then implemented to a variably loaded pneumatic actuator. Simulation and experimental tests are conducted with different inputs, namely, step, multistep, and random waveforms, to evaluate the performance of the proposed technique. The results obtained have been proven as a novel initiative at examining and identifying the characteristic based on a new proposal controller resulting from N-PID controller. The transient response is improved by a factor of 2.2 times greater than previous N-PID technique. Moreover, the performance of pneumatic positioning system is remarkably good under various loads

Feasible, Robust and Reliable Automation and Control for Autonomous Systems

The Special Issue book focuses on highlighting current research and developments in the automation and control field for autonomous systems as well as showcasing state-of-the-art control strategy approaches for autonomous platforms. The book is co-edited by distinguished international control system experts currently based in Sweden, the United States of America, and the United Kingdom, with contributions from reputable researchers from China, Austria, France, the United States of America, Poland, and Hungary, among many others. The editors believe the ten articles published within this Special Issue will be highly appealing to control-systems-related researchers in applications typified in the fields of ground, aerial, maritime vehicles, and robotics as well as industrial audiences

Advanced Strategies for Robot Manipulators

Amongst the robotic systems, robot manipulators have proven themselves to be of increasing importance and are widely adopted to substitute for human in repetitive and/or hazardous tasks. Modern manipulators are designed complicatedly and need to do more precise, crucial and critical tasks. So, the simple traditional control methods cannot be efficient, and advanced control strategies with considering special constraints are needed to establish. In spite of the fact that groundbreaking researches have been carried out in this realm until now, there are still many novel aspects which have to be explored