High-Level Integration Sizing Tool for Electrical Architectures (HighLITE)

<div class="section abstract"><div class="htmlview paragraph">Many More-Electric Aircraft (MEA) Electric Power System (EPS) architecture paradigms are being studied in order to provide the on-board electrical loads with high-quality supply and to ensure safe operation. EPS with dc distribution appears to be more promising due to higher efficiency, higher reliability, easier integration and lower overall weight. Another advantage of dc systems is the ease of sources paralleling, together with the optimization of load power sharing, this can lead to further EPS weight reduction. The DC bus can be fed by multiple sources such as generators, batteries and other energy storage devices.</div><div class="htmlview paragraph">Many loads in MEA EPS are tightly controlled by power electronic converters and often behave as constant power loads (CPL). These are known as main contributors to the degradation of EPS stability margins. Therefore, stability study is one of the key topics in the assessment of potential EPS architecture candidates.</div><div class="htmlview paragraph">This study deals with stability study of an example EPS consisting of two permanent-magnet starter-generators feeding a mixed load. The generators are controlled in flux-weakening mode and they feed the main dc bus with currents according to the droop characteristics. The mathematical model of such EPS is developed and used for detailed stability study. The system eigenvalues contours are investigated with the variation of the key system parameters including bandwidth of main control loops, length of the cables, load power level and others. The achieved analytical results are verified by the time-domain simulations.</div></div>

This paper identifies the most promising electric power system (EPS) architecture for a future more electric aircraft based on reviews and evaluations of both system weight and stability feature of the existing EPS architectures. When comparing the overall system weight of different architectures, various aspects, including voltage generation, wiring system, ground operation, power conversion, and complexity of integrating alternative energy sources, are considered. After choosing the possible candidates among all the possible architectures by using weight-saving criterion, stability features for the initially selected candidates are further evaluated. Necessary simulation studies are carried out in MATLAB/Simulink to prove the correctness of stability study. Finally, the one both good at weight saving and with the highest stability region is deemed as the most promising EPS architecture for future MEAs.

When designing an electric power system (EPS) architecture for a more electric aircraft (MEA), the total weight of the system is treated as one of the most important criteria. For the weight saving purpose, this paper proposes an optimal power flow (OPF) based architecture design method to minimise the redundancy of the EPS of MEA, which includes reducing the generator overloading requirements for lighter generator design, and cutting down the excessive harness and number of contactors to lighten the wiring system. Based on the formulized mixed-integer linear programming (MILP) model, the addressed optimal architecture design (OAD) problem can be solved by optimising the power routing with minimum transmission losses in different flight stages simultaneously to minimise generator sizing and number of connections. The model contains both decision variables indicating the system architecture (e.g. cables existences and generator capacity) and the ones indicating the power flows with regards to the flight stages. In addition, the total transmission losses in the system are considered by formulizing the non-linear transmission losses of the DC/DC converters and cables losses in model constraints. By minimising the transmission losses, the generator overload capacity, as well as the cable needed for the connections, an optimised architecture with less redundancy and having optimal power routing in different flight stages can be realized, leading to lighter generator and wiring system for EPS.

This paper investigates the dynamic stability of a droop-controlled multi-generator system in the more electric aircraft (MEA). Based on the developed state-space model of the potential dc electrical power system (EPS) architecture, the stability boundaries of EPS operation depending on parameter variations including component parameters and operating conditions are investigated. The effect of multiple parametric uncertainties on EPS stability is graphically illustrated by stability regions maps. In addition, the effect of the droop coefficient on the stability is discussed from the impedance point of view. The detailed mathematical models and analytical results of stability assessment are verified by time domain simulation studies.

In this work, the open-source plugin OpenMRH is presented for the Open Robotics Automation Virtual Environment (OpenRAVE), a simulation environment for testing, developing and deploying motion planning algorithms. The proposed plugin allows for a fast and automated generation of different modular hand models. OpenMRH combines virtual-prototyping and modular concepts. Each modular model is generated by applying a dynamically generated code, which is consistent with the standard syntax expected by OpenRAVE for the simulated models. In this way, once the desired model is generated, an instance of OpenRAVE can be launched and the model can be visualised. Alternatively, the modular models can be generated from a user-defined input specified via a graphical user interface (GUI). The generated models can be used for testing, developing and deploying grasp or motion planning algorithms. Two case studies are considered to validate the efficiency of the proposed model generator. In the first case study, a modular robotic hand model is generated with OpenMRH by using user-defined input parameters. In the second case study, another hand model is generated with OpenMRH by using algorithmic defined input parameters.

The electricity demand forecast allows countries to establish long-term plans and objectives for identifying gaps, selecting strategies, and designing the electric power system's architecture. Traditional models use GDP as the primary variable to forecast the electricity demand. The work presents an analysis of the relationship between electricity demand and economic growth, using regression methods with one or more variables. The GDP and sectoral GDP data was provided by Banco de la República de Colombia. The results validate the traditional model and offer alternative models that can relate the economy's different sectors with the electricity demand.

Naval Power (and Energy Systems) Existing Ships MVAC Architectures MVDC Architectures Properties of a Naval Power (and Energy) System Limited rotational inertia — AC frequency is not a constant Lack of Time Scale Separation Load sharing vice Power Scheduling Short electrical distances Load dynamics very important System behavior dominated by controls.

<title>ABSTRACT</title> <p>Electrical power system upgrades needed to fulfill mission objectives for next generation vehicles will require technology advances such as greater power density, increased functionality, and higher operating temperature. To meet these requirements, electrical power demands will exceed the capabilities of currently available low voltage power systems. High Voltage DC (HVDC) systems, e.g., 270 – 800 VDC, are being considered to meet next generation vehicle requirements, but these electrical power systems have the potential for extremely large fault currents in case of electrical equipment failure. Improved battery safety and intelligent Solid State Circuit Breakers (SSCB) and Solid State Power Controllers (SSPC) are needed to improve mission effectiveness, reliability, and personnel safety of next generation military and commercial ground, air, and sea vehicle electrical power systems. In this paper we present three enabling technologies developed by Creare: (1) an intelligent Battery Management System (BMS); (2) a fast-acting Silicon Carbide (SiC) SSCB; and (3) an intelligent SiC SSPC. All three technologies integrate into existing vehicle communications systems via CAN bus to support emerging system level management tools and power system architectures. Modularity and integration with existing and evolving system architectures is achievable through firmware upgrades, e.g., to support Stryker modernization, VICTORY, JLTV, and GCV architectures. The flexibility of these three key technologies provides advanced capabilities for a variety of applications including military and commercial ground, air, and sea vehicles.</p>

Planning carbon emission trading for Beijing's electric power systems under dual uncertainties

Circuit modeling is an essential tool in the design of power electronic applications. Both the onstate forward voltage drop and transient thermal impedance of high power SCRs and diodes are complex functions. The main objective of this paper is how to use modeling equations to evaluate a given power electronic application. The forward on-state forward voltage drop can be modeled by both the classical ABCD and the new MNOP...parameters. The transient thermal impedance has been shown to be well represented via four or five exponential terms representing the significant transient thermal time constants of the device. Both the digital (hard code) simulation and analog PSPICE simulation techniques are described. Also, a new tool, called STARSim, is described. STARSim permits comparison of the older superposition method and new modeling method by performing the calculations using both approaches. A simple SCR model for PSPICE incorporating the on-state forward voltage drop and transient thermal impedance models is also described and evaluated. This information is considered to be important in providing the tools required for power electronic design engineers to quickly evaluate a given device in proposed or existing power electronic application.

CubeSats have been widely used for space research due to lower cost and faster development. The electric power system (EPS) is one of the key subsystems of CubeSat which powers all the other subsystems. One of the important steps in the EPS design is the selection of EPS architecture which should be done considering overall efficiency, battery size, reliability, and simplicity of control. In the literature, a general comparison between different architectures is performed without considering the mission parameters, power generation profile, and load profile based on the operational modes. Thus, the best possible EPS architecture may not be selected in the design phase. Therefore, the main objective of this article is to develop a systematic methodology to compare various peak power tracking EPS architectures of CubeSat in terms of orbital efficiency for all possible modes of operation, component count, reliability, and battery size to meet the required number of cycles of charge/discharge for the given mission duration. The proposed methodology has been demonstrated using the real data and scenarios of MYSAT-1, which is a 1U CubeSat developed and launched by Khalifa University. The results demonstrate that EPS architecture with series-connected maximum power tracking converters for solar panels and unregulated dc-bus has the highest efficiency for all operating modes, lower component count, higher reliability, and minimum battery capacity or longer lifetime for the same battery specifications.

The Electric Power System (EPS) being built for the International Space Station has undergone several significant changes over the last year, as major design decisions have been made for the overall station. While the basic topology and system elements have remained the same, there are important differences in connectivity, assembly sequence, and start-up. The key drivers for these changes in architecture have been the goal to simplify verification, and most significantly, the introduction of extensive Russian participation in the program. Having the Russians join the international community in this project has resulted in an expanded station size, larger crew, and almost doubled the observable surface of the Earth covered by the station. For the power system it has meant additional interfaces for power transfer, and new challenges for solar tracking at the higher inclination orbit. This paper reviews the current architecture and emphasizes the new features that have evolved, as the design for the new, larger station has developed. Additionally, the possible application of developing technology to the station, and other future missions is considered.

Welcome to the DATE 08 Conference Proceedings. DATE combines the world's favourite electronic systems design conference and Europe's leading international exhibition for electronic design, automation and test, from system level hardware and software implementation right down to integrated circuit design. The DATE 08 event features a technical program with 77 sessions covering the latest developments in system design and embedded software, IC design/test methodologies and EDA tools, together with an exhibition with the leading EDA, silicon and IP providers showing their new products and services. Challenges that you all face or soon will face in your daily practice are the increasing design complexity of highly integrated systems, the introduction of reconfigurability and embedded software, and the control of power and variability in nanometer IC designs. All these issues will be addressed in this year's DATE event. For the 11th successive year DATE has prepared an exciting technical programme, with the help of the more than 400 members of the Technical Programme Committee, who dedicated their time to thoroughly review the 839 submissions in 37 topics, ranging from system level down to circuit design and covering all the most relevant application domains. The submissions are organised in 4 major areas: D --- Design Methods, Tools, Algorithms and Languages A --- Application Design T --- Test Methods, Tools and Innovative Experiences E --- Embedded Software After a thorough review and selection process (with an average of 5 reviews per paper), finally 198 regular papers were selected for presentation at the conference. Additionally, there are 46 Interactive Presentations that are organised in 5 IP sessions. Together with the invited special sessions (panels, embedded tutorials and hot topic sessions), this has resulted in a high-quality technical program. The technical program provides a wide but high-quality coverage of design, design automation and test topics, from the system level to the integrated circuit level. Compared with previous years, submissions in the Embedded Software track has increased by 50%, showing a clear trend towards a comprehensive system design focus with integrated hardware and software solutions. DATE has established itself firmly as a true Electronic System Design Conference. This year the conference is held in Germany, at the ICM in Munich and spans an entire working week from Monday March 10 to Friday March 14. On Monday, eleven pre-conference tutorials will be given. The three-full day tutorials cover topics of great interest for system design. The first tutorial deals with techniques to automatically realising embedded system from high-level functional models. The second tutorial addresses the different issues related to communication based design and architectures in automotive electronic systems. The third tutorial discusses several key concepts on system-level design and application mapping for wireless and multimedia MPSoC architectures. Furthermore, eight half-day tutorials are also given, which cover a wide spectrum of topics on specification, modelling, design and test. The main conference opens on Tuesday March 11, with two very interesting and complementary keynote speeches. Dominique Vernay, Chief Technical Officer for Thales, will talk about the challenges of embedded systems design, and Giovanni de Micheli, Professor at EPFL, will present his views on designing micro/nano systems for a safer and healthier tomorrow. On the same day, the Executive Track offers a series of business panels with executives discussing hot topics in design: the perils of 45 nanometers, the changes in EDA strategies from IDM, to fablite to fabless, and embedded systems level design strategies. DATE 08 will again offer two specific days related to special themes. On Wednesday March 12, a special full-day track is devoted to Automotive Electronics---Software and Architecture. This special-day track will focus on the challenges faced by the automotive supply chain with particular attention to system and software architecture design. It provides a comprehensive analysis of the evolution of automotive architectures, including ECUs, sensors and communication standards and discusses how new methods, tools and standards for interoperability and component-based design can deal with the increasing complexity of software systems and their need for reliability and guaranteed timely behaviour. In addition, it addresses to what degree existing standards, including AUTOSAR and FLEXRAY and model-based development, can support the development of safety and time-critical software. On Thursday March 13, a second special full-day track focuses on Dependable Embedded Systems. This track will address both conceptual and applied issues for design, analysis and validation of dependable embedded systems. The utility of embedded systems and services is based, in large part, on our depending on their sustained functionality in spite of the encountered operational or malicious disruptions. As the number of transient and also permanent disruptions (given the decreasing device geometries, higher device density, lower voltage latching, faster clocks etc) is expected to increase substantially, this will not only be a key issue for the hardware community but also the systems community in general. Solutions using a combination of hardware and software might be more effective than hardware-only or software-only solutions. This track focuses on both conceptual and applied issues for design, analysis and validation of dependable embedded systems. Besides these special tracks, the main conference is organized in six parallel tracks of sessions, three devoted to design methods, tools, algorithms and languages, one to application design, one to test methods, tools and innovative experiences, and finally one to embedded software. The presentations of the selected regular papers in these parallel tracks are complemented by nine Special Sessions and two Invited Industrial Sessions. The special sessions are organized in the form of panels, hot topics, and embedded tutorials. The topics to be covered include quantitative evaluation for embedded systems design, design and manufacturing at 32 and 22nm, software for wireless networked embedded systems, test challenges for low power devices, quantitative productivity measurement in IC design, and 3D Integration. The two invited industrial sessions deal with industrial system designs in transportation and information technologies. To emphasise that DATE is the major event for the designers, DATE 08 features also invited sessions where Europe's famous consumer industry presents their best designs and design practices. Friday March 14 is the day for the DATE workshops. DATE 08 offers workshops on current and emerging important issues in design, test, EDA and software to complement the regular conference. They provide a unique opportunity for the various research and design communities to spend a day discussing the latest and the best, sharing their experiences and visions. This year's workshop program includes eight workshop themes. Four workshops are related to software engineering, ranging from dependable software to modelling, analysis and development tools. Four other workshop themes cover a variety of topics such as the impact of process variations on design and test, the merging world of Nano-Electro-Mechanical Systems, new directions in high level synthesis, and heterogeneous reconfigurable hardware. Each workshop features presentations, invited or submitted, from highly distinguished academic and industrial researchers. Finally, throughout the conference days, DATE offers a comprehensive overview of commercial design and verification tools in its large exhibition hall. Exhibitors include EDA vendors, silicon, FPGA and IP providers showing their new products and services. In addition, there is an Exhibition Theatre featuring talks from engineering managers of the leading electronic manufacturers on first-hand design experiences of commercial EDA tools. New this year is the European projects village where different European and large government funded projects will be able to show their ongoing research and results to the design community and have the opportunity for internal meetings and discussions. The DATE week will be also an opportunity for students and universities to show their research work, through the PhD Forum on Monday evening and the University Booth where hardware and software demonstrations will be shown by different universities on a rotation schedule. The DATE 08 event's program will be particularly attractive to industrial designers, at analog, IC, FPGA and embedded system level, as well as software designers, to researchers and academics as well as to design managers, and an increasing attendance is expected. We therefore invite you to take full advantage of the many opportunities offered to you by DATE 08, to extend your knowledge and/or business in electronic system's design and to exploit the abundant networking possibilities offered to socialise with colleagues, including fringe meetings and a memorable social party with bands and dancing. We hope that you will all enjoy the DATE 08 Conference and Exhibition.

Data analytics is a key factor to make fully informed and data-driven decisions in modern manufacturing companies. With increasing international competition, classical approaches to data analytics have to be enhanced toward advanced data analytics to create smarter products, production processes and customer services. This leverages the full potential of the data to quickly gain insights and make decisions. Application areas include predictive analytics, augmented analytics and real-time analytics. In this paper an advanced data analytics platform (ADAP) for manufacturing companies is presented and verified on a real-world production line. ADAP combines process data obtained in a physical environment with domain knowledge from experts to create data-driven models in a digital environment. In addition, ADAP is well scalable and provides a comprehensible data structure throughout the entire data workflow. ADAP is verified on two different advanced data analytics applications on an electrocoating plant. In order to relate the applications to real production requirements, the needs of local manufactures from the region Ostwestfalen-Lippe (OWL) are taken into account.

The development of a scalable and user-friendly SPICE model is a key aspect of exploring the potential of spin-transfer torque MRAM (STT-MRAM). A self-contained magnetic tunnel junction (MTJ) SPICE model is proposed in this work which can reproduce realistic MTJ characteristics based on user-defined input parameters such as the free layer's length, width, and thickness. Using the propose model, scalability studies of both in-plane and perpendicular MTJs can be performed across different technology nodes with minimal effort, which differentiates this model from most previously reported models.