Design tool

About: Design tool is a research topic. Over the lifetime, 3864 publications have been published within this topic receiving 46401 citations.

Modeling and design optimization of ReRAM

Abstract: Resistive switching memories (ReRAM) have been widely studied for applications in next-generation data storage and neurormorphic computing systems. To enable device-circuit-system co-design and optimization, a SPICE model of ReRAM that can reproduce the device characteristics in circuit simulations is needed. In this paper, we present a novel tool for ReRAM design including a physics-based SPICE model, the model parameters extraction strategy, as well as the system assessment method. This physics-based SPICE model can capture all the essential features of HfO x -based ReRAM including the DC/AC and multi-level switching behaviors, switching reliability, and intrinsic device variations. A strategy is developed to extract the critical model parameters from the fabricated ReRAM devices. A variety of electrical measurements on various ReRAMs are performed to verify and calibrate the model. The assessment method based on the experimentally verified SPICE model can be applied to explore a wide range of applications including: 1) variation-aware and reliability-emphasized system design; 2) system performance evaluation; 3) array architecture optimization. This verified design tool not only enables system design but also enables system optimization that capitalizes on device/circuit interaction for both data storage and neuromorphic computing applications.

Multidisciplinary Optimization of Aeronautical Systems

Abstract: T special section (this issue and the Jan. 1991 issue) on Multidisciplinary Optimization of Aeronautical Systems comes nearly a decade after Holt Ashley surveyed the same subject in a now-classic Wright Brothers Lecture (published in this journal in Jan. 1982). It was a decade of vigorous development from which optimization emerged as a new methodology applicable at all levels and in each phase of the aircraft design process. The papers in this section are representative of the accomplishments and themes of that decade of progress. Most of the papers were invited by editors and cover a wide range of topics including optimization methodology, sensitivity analysis, algorithms synthesis and efficiency, comprehensive codes, and applications to systems. The objective of this collection of papers is to highlight the potential of optimization as a powerful design tool to the aerospace community. The scope of optimization methodology is expanding rapidly to solve multidisciplinary system problems for both preliminary and detailed designs. In fact, many of the papers discuss application to full-scale practical problems. At the philosophical level, the notion of "the push button design" that underpinned some early attempts at creating optimization programs of unlimited applicability gave way to a more mature view of the numerical optimization role in design. The view is founded in the recognition of the design as an activity which intrinsically blends the qualitative, judgmental, and creative side with the qualitative, precise, and algorithmic side. Without prejudging the future progress of "artificial intelligence," it is obvious for now that it is the algorithmic, numerical side that may benefit the most from the computerbased optimization methods. The perceived need is also the strongest for that category of methods because they liberate engineers from a tedium as contrasted with the creative side of design. Not surprisingly, then, most of the papers in this section concentrate primarily on the quantitative category of methods. At the application level, the user demand that drives the optimization development has been intensifying because of the following: 1) Major new aircraft design projects have become fewer and farther apart in time, hence past experience becomes less useful as a guide in making the design decisions. 2) Advanced aircraft tend to be enormously complex systems of interconnecting parts and disciplines, and ultimate performance hinges on the myriad of numerical interplays, some of them very subtle and beyond the power of human judgment to evaluate precisely. 3) Young engineers who have grown up with computers enter the work force feeling very comfortable working with the machine that has been their friend since early adolescence. 4) Data processing capability of modern computers has increased enormously. The challenge posed by the advanced aircraft as a complex system was taken up by the development of decomposition methods that break the large intractable problem into smaller subproblems while maintaining the couplings among the subproblems. In the design office, this approach maps well onto the natural organization of engineering into groups by disciplinary and task specializations. It preserves and nurtures the advantages of the division of labor, including the concurrence of operations—the time-honored principle of industrial management first articulated by Adam Smith in the classic work The Wealth of Nations nearly 250 years ago. The decomposition approach stems also from the realization that the sensitivity analysis that generates data for optimization algorithms may easily account for more than 90% of the total computational cost. Hence, the recent emphasis on efficient sensitivity analysis applicable to complex systems appears justified. The notion of decomposition is represented in this issue both at the theoretical level and at the level of application to aircraft configuration optimization. Various decomposition schemes and their applications presented in this volume have one common feature: each offers a particular pattern that unifies the analysis, sensitivity analysis, and optimization itself in a modular framework, whose overall logical structure is problem-independent even though its modules may be so dependent. An ancillary benefit from this is a clear description for each module of its function in the broad scheme of things and of the input and output on which it is expected to operate. This information amounts to the specifications that should aid in future developments of such modules. The rapid increase in capability of the specialized optimization methods that might be regarded as modules in the above system perspective is evident in the collection—primarily in the papers of structural optimization, aeroelastic optimization, and synthesis of active control. It is apparent that recent progress has brought about a quantum improvement in comprehensiveness of the problems formulation and application robustness. The next logical step will be to bring these modular capabilities into the decomposition-based procedures for overall aircraft optimization. Several papers in this collection concern the application of optimization methodology to helicopter systems. The helicopter is a truly multidisciplinary system, and its dynamics, aerodynamics, controls, and flight mechanics are highly coupled. Most of the governing phenomena are inherently nonlinear and very involved. It is therefore a challenging task to apply an optimization methodology in a helicopter system to reduce vibration and blade stresses and to improve performance and rotor stability. The dictates of passenger comfort, reduced operating cost, and capabilities to achieve expanding future missions necessitate the search for optimized designs. There are growing optimization activities, and many innovative ideas are emerging that will help build improved helicopters in the future. One should note that the content of this special section reveals also some deficiencies that need to be corrected in the near future in order to make the above procedures complete. The underrepresentation of aerodynamic optimization and propulsion optimization in the collection points to such obvious deficiencies. Another apparent deficiency is that the tailorability of structural characteristics including couplings

Computer-aided design of power electronic circuits

Abstract: The general purpose circuit simulation package SPICE is used as a design tool for power electronic circuits. The process involves simulation of the complete circuit in the microsecond timescale, by which circuit behaviour under different operating conditions can be studied. Semiconductor device models and interconnection inductances are examined. The simulation process is applied to a 50 kVA transistorised chopper circuit and the results are discussed and compared with experimental results.

A design tool for efficient mapping of multimedia applications onto heterogeneous platforms

Abstract: Development of multimedia systems on heterogeneous platforms is a challenging task with existing design tools due to a lack of rigorous integration between high level abstract modeling, and low level synthesis and analysis. In this paper, we present a new dataflow-based design tool, called the targeted dataflow interchange format (TDIF), for design, analysis, and implementation of embedded software for multimedia systems. Our approach provides novel capabilities, based on the principles of task-level dataflow analysis, for exploring and optimizing interactions across application behavior; operational context; heterogeneous platforms, including high performance embedded processing architectures; and implementation constraints.

Wind turbine design using a free-wake vortex method with winglet application

Abstract: Wind turbine blades are traditionally designed with blade element momentum theory (BEMT). This method is incapable of accurately analyzing non-conventional or non-planar blade planforms. Modern wind turbine blade design thus requires non-standard modeling that can effectively analyze the effects of a non-planar blade, such as a blade with a winglet. The free-wake, distributed vorticity element (FW-DVE) method meets these analysis goals. Previous work applied the FW-DVE method to wind turbines, but this work did not include the influence of profile forces and did not include any design applications. The present research focused on developing the FW-DVE method into a design tool for wind turbine design applications and on the validation of this tool. In the research presented in this thesis, the FW-DVE method was modified to include the effect of airfoil profile drag and to account for the effects of stall and a non-linear lift-curve. A design tool was created to aid in using the WindDVE analysis code for trade space exploration. The method was used to analyze and design a winglet for a small-scale wind turbine, which was tested in a wind tunnel at the University of Waterloo where it exhibited a 9% increase in the maximum coefficient of power of the rotor. The performance results from this test have been used to validate the FW-DVE method for wind turbine design, along with an analysis of the National Renewable Energy Laboratory’s Unsteady Aerodynamics Experiment Phase VI wind turbine.