52 resultados para Uninterruptable Power Supply


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El origen del proyecto se encuentra en la mejora de un inversor trifásico sinusoidal comercial sobre la base del estudio de las técnicas de excitación óptimas para los IGBTs que lo componen en su etapa de potencia. En las primeras fases de planteamiento del proyecto se propone una idea mucho más ambiciosa, la realización de un nuevo convertidor de emergencia, destinado al sector ferroviario, para dar servicio de climatización. Este convertidor está formado por la asociación en cascada de un bloque DC/DC elevador y un bloque inversor DC/AC trifásico controlado mediante PWM con modulación sinusoidal. Se pretendía así dar solución a las siguientes problemáticas detectadas en los convertidores comercializados hasta el momento: un bloque elevador excesivamente sobredimensionado, subsistemas de control independientes para los dos bloques que configuran el convertidor, adicionalmente, la tarjeta driver se rediseña con cada cambio de especificaciones por parte de un nuevo cliente y finalmente, las comunicaciones tanto de diagnosis como de mantenimiento necesitaban una importante actualización. Inicialmente, se ha realizado un estudio teórico de los bloques elevador e inversor para poder realizar el diseño y dimensionamiento de sus componentes tanto semiconductores como electromagnéticos. Una vez completada la parte de potencia, se estudia el control que se realiza mediante medidas directas y simulación tanto de la estrategia de control del elevador como del inversor. Así se obtiene una información completa de la funcionalidad de las tarjetas existentes. Se desea realizar el diseño de una única tarjeta controladora y una única tarjeta de drivers para ambos bloques. Por problemas ajenos, en el transcurso de este proyecto se cancela su realización comercial, con lo que se decide al menos crear la placa de control y poder gobernar un convertidor ya existente, sustituyendo la tarjeta de control del bloque elevador. Para poder fabricar la placa de control se divide en dos tarjetas que irán conectadas en modo sándwich. En una tarjeta está el microcontrolador y en otra está todo el interface necesario para operar con el sistema: entradas y salidas digitales, entradas y salidas analógicas, comunicación CAN, y un pequeño DC/DC comercial que proporciona alimentación al prototipo. Se realiza un pequeño programa funcional para poder manejar el convertidor, el cual con una tensión de 110V DC, proporciona a la salida una tensión de 380V AC. Como ya se ha expuesto, debido a la cancelación del proyecto industrial no se profundiza más en su mejora y se decide proponerlo para su evaluación en su fase actual. ABSTRACT. The beginning of the project is found in the improvement of a commercial sine wave three phase inverter which is based in a study about optimal excitation techniques to IGBTs which compose in the power stage. In the early phases of project it is proposed a much more ambitious idea, the fact of a new emergency converter, proposed for the rail sector to work in an air condition unit. This converter is formed by an association of a block cascaded DC/DC booster and a block DC/AC inverter three-phase controlled by a sine wave modulation PWM. The purposed was to give a solution to following problems detected in commercial converters nowadays: an excessively oversized block boost, independent control subsystems for two blocks that configure the converter. In addition, driver board is redesigned with each specifications change demand it a new customer, and finally, the communications, diagnostic and maintenance that needed a important upgrade. Initially, it has been performed a theoretical study of boost and the inverter blocks to be able to perform the component’s design and the size (semiconductor and electromagnetic fields). Once finished power study, it is analysed the control performed using direct measures and simulation of boost control strategy and inverter. With this it is obtained complete information about existing cards functionality. The project is looking for the design of just one controller card and one drivers´ card for both blocks. By unrelated problems, during the course of this project a commercial realization. So at least its decided to create control board to be able to existing converter, replacing boost block’s control board. To be able to manufacture control board it is divided in two cards connected in sandwiching mode. In a card is microcontroller and in another is all needed interface to operate with the system: digital inputs and outputs, analogical inputs and outputs, CAN communication, and a small DC / DC business that provide power supply to the prototype. It is performed a small functional program to handle the converter, which with an input voltage 110V DC provides an output voltage 380V AC. As already has been exposed, due to industrial project cancellation it is decided no to continue with all improvements and directly to evaluate it in the current phase.

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La medición y testeo de células fotovoltaicas en el laboratorio o en la industria exige reproducir unas condiciones de iluminación semejantes a las reales. Por eso se utilizan sistemas de iluminación basados en lámparas flash de Xenon que reproducen las condiciones reales en cuanto a nivel de irradiancia y espectro de la luz incidente. El objetivo de este proyecto es realizar los circuitos electrónicos necesarios para el disparo de dichas lámparas. El circuito de alimentación y disparo de una lámpara flash consta de una fuente de alimentación variable, un circuito de disparo para la ionización del gas Xenon y la electrónica de control. Nuestro circuito de disparo pretende producir pulsos adecuados para los dispositivos fotovoltaicos tanto en irradiancia, espectro y en duración, de forma que con un solo disparo consigamos el tiempo, la irradiancia y el espectro suficiente para el testeo de la célula fotovoltaica. La mayoría de estos circuitos exceptuando los específicos que necesita la lámpara, serán diseñados, simulados, montados en PCB y comprobados posteriormente en el laboratorio. ABSTRACT. Measurement and testing of photovoltaic cells in the laboratory or in industry requires reproduce lighting conditions similar to the real ones. So are used based lighting systems xenon flash lamps that reproduce the actual conditions in the level of irradiance and spectrum of the incident light. The objective of this project is to make electronic circuits required for such lamps shot. The power supply circuit and flash lamp shot consists of a variable power supply, a trigger circuit for Xenon gas ionization and the control electronics. Our shot circuit aims to produce pulses suitable for photovoltaic devices both irradiance, spectrum and duration, so that with a single shot get the time, the irradiance and spectrum enough for testing the photovoltaic cell. Most of these circuits except lamp specific requirements will be designed, simulated, and PCB mounted subsequently tested in the laboratory.

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Resulta difícil definir una profesión que surge por la necesidad de adaptar los espacios de trabajo a las nuevas tendencias de las organizaciones, a la productividad, a las nuevas tecnologías que continúan modificando y facilitando desde las últimas décadas el modo y forma de trabajar. Mucho más complicado resulta definir una profesión casi invisible. Cuando todo funciona en un edificio, en un inmueble, en un activo. Todo está correcto. He ahí la dificultad de su definición. Lo que no se ve, no se valora. Las reuniones, las visitas, un puesto de trabajo, una sala de trabajo, una zona de descanso. La climatización, la protección contra incendios, la legionela, el suministro eléctrico, una evacuación. La organización, sus necesidades, su filosofía. Los informes, los análisis, las mejoras. Las personas, el espacio, los procesos, la tecnología. En la actualidad, todo se asocia a su coste. A su rentabilidad. En la difícil tarea de realizar el proyecto de un edificio, participan multitud de aspectos que deben estar perfectamente organizados. El arquitecto proyecta y aúna en el proyecto: pasado (experiencia), presente (tendencias) y futuro (perdurabilidad). Y es en ese momento, cuando al considerar el futuro del edificio, su perdurabilidad, hace que su ciclo de vida sea criterio fundamental al proyectar. Que deba considerarse desde el primer esbozo del proyecto. Para que un edificio perdure en el tiempo existen gran número de factores condicionantes. Empezando por su uso apropiado, su nivel de actividad, pasando por las distintas propiedades que pueda tener, y terminando por los responsables de su mantenimiento en su día a día. Esa profesión invisible, es la disciplina conocida como Facility Management. Otra disciplina no tan novedosa –sus inicios fueron a finales del siglo XIX-, y que en la actualidad se empieza a valorar en gran medida es la Responsabilidad Social. Todo lo que de forma voluntaria, una organización realiza por encima de lo estrictamente legal con objeto de contribuir al desarrollo sostenible (económico, social y medio ambiental). Ambas disciplinas destacan por su continuo dinamismo. Reflejando la evolución de distintas inquietudes: • Personas, procesos, espacios, tecnología • Económica, social, medio-ambiental Y que sólo puede gestionarse con una correcta gestión del cambio. Elemento bisagra entre ambas disciplinas. El presente trabajo de investigación se ha basado en el estudio del grado de sensibilización que existe para con la Responsabilidad Social dentro del sector de la Facility Management en España. Para ello, se han estructurado varios ejercicios con objeto de analizar: la comunicación, el marco actual normativo, la opinión del profesional, del facilities manager. Como objetivo, conocer la implicación actual que la Responsabilidad Social ejerce en el ejercicio de la profesión del Facilities Manager. Se hace especial hincapié en la voluntariedad de ambas disciplinas. De ahí que el presente estudio de investigación realice dicho trabajo sobre elementos voluntarios y por tanto sobre el valor añadido que se obtiene al gestionar dichas disciplinas de forma conjunta y voluntaria. Para que una organización pueda desarrollar su actividad principal –su negocio-, el Facilities Manager gestiona el segundo coste que esta organización tiene. Llegando a poder ser el primero si se incluye el coste asociado al personal (nóminas, beneficios, etc.) Entre el (70 – 80)% del coste de un edificio a lo largo de toda su vida útil, se encuentra en su periodo de explotación. En la perdurabilidad. La tecnología facilita la gestión, pero quien gestiona y lleva a cabo esta perdurabilidad son las personas en los distintos niveles de gestión: estratégico, táctico y operacional. En estos momentos de constante competencia, donde la innovación es el uniforme de batalla, el valor añadido del Facilities Manager se construye gestionando el patrimonio inmobiliario con criterios responsables. Su hecho diferenciador: su marca, su reputación. ABSTRACT It comes difficult to define a profession that emerges due to the need of adapting working spaces to new organization’s trends, productivity improvements and new technologies, which have kept changing and making easier the way that we work during the last decades. Defining an invisible profession results much more complicated than that, because everything is fine when everything works in a building, or in an asset, properly. Hence, there is the difficulty of its definition. What it is not seen, it is not worth. Meeting rooms, reception spaces, work spaces, recreational rooms. HVAC, fire protection, power supply, legionnaire’s disease, evacuation. The organization itself, its needs and its philosophy. Reporting, analysis, improvements. People, spaces, process, technology. Today everything is associated to cost and profitability. In the hard task of developing a building project, a lot of issues, that participate, must be perfectly organized. Architects design and gather/put together in the project: the past (experience), the present (trends) and the future (durability). In that moment, considering the future of the building, e. g. its perdurability, Life Cycle turn as the key point of the design. This issue makes LCC a good idea to have into account since the very first draft of the project. A great number of conditioner factors exist in order to the building resist through time. Starting from a suitable use and the level of activity, passing through different characteristics it may have, and ending daily maintenance responsible. That invisible profession, that discipline, is known as Facility Management. Another discipline, not as new as FM –it begun at the end of XIX century- that is becoming more and more valuable is Social Responsibility. It involves everything a company realizes in a voluntary way, above legal regulations contributing sustainable development (financial, social and environmentally). Both disciplines stand out by their continuous dynamism. Reflecting the evolution of different concerning: • People, process, spaces, technology • Financial, social and environmentally It can only be managed from the right change management. This is the linking point between both disciplines. This research work is based on the study of existing level of increasing sensitivity about Social Responsibility within Facility Management’s sector in Spain. In order to do that, several –five- exercises have been studied with the purpose of analyze: communication, law, professional and facility manager’s opinions. The objective is to know the current implication that Social Responsibility has over Facility Management. It is very important the voluntary part of both disciplines, that’s why the present research work is focused over the voluntary elements and about the added value that is obtained managing the before named disciplines as a whole and in voluntary way. In order a company can develop his core business/primary activities, facility managers must operate the second largest company budget/cost centre. Being the first centre cost if we considerer human resources’ costs included (salaries, incentives…) Among 70-80% building costs are produced along its operative life. Durability Technology ease management, but people are who manage and carry out this durability, within different levels: strategic, tactic and operational. In a world of continuing competence, where innovation is the uniform for the battle, facility manager’s added value is provided managing company’s real estate with responsibility criteria. Their distinguishing element: their brand, their reputation.

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Use of a conductive bare tape electrically floating in low Earth orbit as an effective electron beam source to produce artificial auroral effects, free of problems that mard tandard beams, is considered. Ambient ions impacting the tape with keV energies over most of its length liberate secondary electrons that race down the magnetic field, excite neutrals in the E layer, and result in auroral emissions. The tether would operate with both a power supply and a plasma contactor off at nighttime; power and contactor would be on at daytime for reboost. Tomographic analysis of auroral emissions from the footprint of the beam, as observed from the spacecraft, can provide density profiles of dominant neutral species in the E layer. A characteristic tether system, at altitude 300 km and moderate orbital inclination, would involve an aluminum tape with a length of 20 km, a width of 15 mm, and a thickness of 0.2 mm for a full-system mass around 1200 kg, with two thirds going into the power subsystem.

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Systems used for target localization, such as goods, individuals, or animals, commonly rely on operational means to meet the final application demands. However, what would happen if some means were powered up randomly by harvesting systems? And what if those devices not randomly powered had their duty cycles restricted? Under what conditions would such an operation be tolerable in localization services? What if the references provided by nodes in a tracking problem were distorted? Moreover, there is an underlying topic common to the previous questions regarding the transfer of conceptual models to reality in field tests: what challenges are faced upon deploying a localization network that integrates energy harvesting modules? The application scenario of the system studied is a traditional herding environment of semi domesticated reindeer (Rangifer tarandus tarandus) in northern Scandinavia. In these conditions, information on approximate locations of reindeer is as important as environmental preservation. Herders also need cost-effective devices capable of operating unattended in, sometimes, extreme weather conditions. The analyses developed are worthy not only for the specific application environment presented, but also because they may serve as an approach to performance of navigation systems in absence of reasonably accurate references like the ones of the Global Positioning System (GPS). A number of energy-harvesting solutions, like thermal and radio-frequency harvesting, do not commonly provide power beyond one milliwatt. When they do, battery buffers may be needed (as it happens with solar energy) which may raise costs and make systems more dependent on environmental temperatures. In general, given our problem, a harvesting system is needed that be capable of providing energy bursts of, at least, some milliwatts. Many works on localization problems assume that devices have certain capabilities to determine unknown locations based on range-based techniques or fingerprinting which cannot be assumed in the approach considered herein. The system presented is akin to range-free techniques, but goes to the extent of considering very low node densities: most range-free techniques are, therefore, not applicable. Animal localization, in particular, uses to be supported by accurate devices such as GPS collars which deplete batteries in, maximum, a few days. Such short-life solutions are not particularly desirable in the framework considered. In tracking, the challenge may times addressed aims at attaining high precision levels from complex reliable hardware and thorough processing techniques. One of the challenges in this Thesis is the use of equipment with just part of its facilities in permanent operation, which may yield high input noise levels in the form of distorted reference points. The solution presented integrates a kinetic harvesting module in some nodes which are expected to be a majority in the network. These modules are capable of providing power bursts of some milliwatts which suffice to meet node energy demands. The usage of harvesting modules in the aforementioned conditions makes the system less dependent on environmental temperatures as no batteries are used in nodes with harvesters--it may be also an advantage in economic terms. There is a second kind of nodes. They are battery powered (without kinetic energy harvesters), and are, therefore, dependent on temperature and battery replacements. In addition, their operation is constrained by duty cycles in order to extend node lifetime and, consequently, their autonomy. There is, in turn, a third type of nodes (hotspots) which can be static or mobile. They are also battery-powered, and are used to retrieve information from the network so that it is presented to users. The system operational chain starts at the kinetic-powered nodes broadcasting their own identifier. If an identifier is received at a battery-powered node, the latter stores it for its records. Later, as the recording node meets a hotspot, its full record of detections is transferred to the hotspot. Every detection registry comprises, at least, a node identifier and the position read from its GPS module by the battery-operated node previously to detection. The characteristics of the system presented make the aforementioned operation own certain particularities which are also studied. First, identifier transmissions are random as they depend on movements at kinetic modules--reindeer movements in our application. Not every movement suffices since it must overcome a certain energy threshold. Second, identifier transmissions may not be heard unless there is a battery-powered node in the surroundings. Third, battery-powered nodes do not poll continuously their GPS module, hence localization errors rise even more. Let's recall at this point that such behavior is tight to the aforementioned power saving policies to extend node lifetime. Last, some time is elapsed between the instant an identifier random transmission is detected and the moment the user is aware of such a detection: it takes some time to find a hotspot. Tracking is posed as a problem of a single kinetically-powered target and a population of battery-operated nodes with higher densities than before in localization. Since the latter provide their approximate positions as reference locations, the study is again focused on assessing the impact of such distorted references on performance. Unlike in localization, distance-estimation capabilities based on signal parameters are assumed in this problem. Three variants of the Kalman filter family are applied in this context: the regular Kalman filter, the alpha-beta filter, and the unscented Kalman filter. The study enclosed hereafter comprises both field tests and simulations. Field tests were used mainly to assess the challenges related to power supply and operation in extreme conditions as well as to model nodes and some aspects of their operation in the application scenario. These models are the basics of the simulations developed later. The overall system performance is analyzed according to three metrics: number of detections per kinetic node, accuracy, and latency. The links between these metrics and the operational conditions are also discussed and characterized statistically. Subsequently, such statistical characterization is used to forecast performance figures given specific operational parameters. In tracking, also studied via simulations, nonlinear relationships are found between accuracy and duty cycles and cluster sizes of battery-operated nodes. The solution presented may be more complex in terms of network structure than existing solutions based on GPS collars. However, its main gain lies on taking advantage of users' error tolerance to reduce costs and become more environmentally friendly by diminishing the potential amount of batteries that can be lost. Whether it is applicable or not depends ultimately on the conditions and requirements imposed by users' needs and operational environments, which is, as it has been explained, one of the topics of this Thesis.

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An electrodynamic tether experiment, to be carried out in the Russian spacecraft Almaz, is proposed. A 10 km tether would be deployed downwards; the lower 8 km would be nonconductive, the upper 2 km would be conductive, bare, and 2.2 mm in diameter, and would act as a thruster, with power supply at the top. This hybrid arrangement allows for other, onelectrodynamic experiments,reducing costs; it also limits the induced electromotive force, reducing the power to be handled. The current-voltage characteristic of contactors would be measured. With the anode switched off, the wire itself should collect a current over 5 A at day conditions, providing a thrust of 0.11 N at a 0.77 kW power.

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An electrically floating bare tether in LEO orbit may serve as upper atmospheric probe. Ambient ions bombard the negatively biased tether and liberate secondary electrons, which accelerate through the same voltage to form a magnetically guided planar e-beam resulting in auroral effects at the E-layer. This beam is free from the S/C charging and plasma interaction problems of standard e-beams. The energy flux is weak but varies accross the large beam cross section, allowing continuous observation from the S/C. A brightness scan of line-integrated emissions, that mix emitting altitudes and tether points originating the electrons, is analysed. The tether is magnetically dragged at nighttime operation, when power supply and plasma contactor at the S/C are off for electrical floating; power and contactor are on at daytime for partial current reversal, resulting in thrust. System requirements for keeping average orbital height are discussed.

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ED bare theters are best systems to deorbit S/C at end of service. For near polar orbits, usual tethers kept vertical by the gravity gradient, yield too weak magnetic drag. Here we propose keeping tethers perpendicular to the orbital plane. they mus be rigid and short for structural reasons, requiring power supply like Ion thrusters. terher tube-booms that can be rolled up on a drum would lie on each side of the S/C. One boom, carying in idle Hollow Cathode, collects electrons; the opposite boom's HC ejects electrons.

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An ED-tether mission to Jupiter is presented. A bare tether carrying cathodic devices at both ends but no power supply, and using no propellant, could move 'freely' among Jupiter's 4 great moons. The tour scheme would have current naturally driven throughout by the motional electric field, the Lorentz force switching direction with current around a 'drag' radius of 160,00 kms, where the speed of the jovian ionosphere equals the speed of a spacecraft in circular orbit. With plasma density and magnetic field decreasing rapidly with distance from Jupiter, drag/thrust would only be operated in the inner plasmasphere, current being near shut off conveniently in orbit by disconnecting cathodes or plugging in a very large resistance; the tether could serve as its own power supply by plugging in an electric load where convenient, with just some reduction in thrust or drag. The periapsis of the spacecraft in a heliocentric transfer orbit from Earth would lie inside the drag sphere; with tether deployed and current on around periapsis, magnetic drag allows Jupiter to capture the spacecraft into an elliptic orbit of high eccentricity. Current would be on at succesive perijove passes and off elsewhere, reducing the eccentricity by lowering the apoapsis progressively to allow visits of the giant moons. In a second phase, current is on around apoapsis outside the drag sphere, rising the periapsis until the full orbit lies outside that sphere. In a third phase, current is on at periapsis, increasing the eccentricity until a last push makes the orbit hyperbolic to escape Jupiter. Dynamical issues such as low gravity-gradient at Jupiter and tether orientation in elliptic orbits of high eccentricity are discussed.

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A 3-year Project started on November 1 2010, financed by the European Commision within the FP-7 Space Program, and aimed at developing an efficient de-orbit system that could be carried on board by future spacecraft launched into LEO, will be presented. The operational system will deploy a thin uninsulated tape-tether to collect electrons as a giant Langmuir probe, using no propellant/no power supply, and generating power on board. This project will involve free-fall tests, and laboratory hypervelocity-impact and tether-current tests, and design/Manufacturing of subsystems: interface elements, electric control and driving module, electron-ejecting plasma contactor, tether-deployment mechanism/end-mass, and tape samples. Preliminary results to be presented involve: i) devising criteria for sizing the three disparate tape dimensions, affecting mass, resistance, current-collection, magnetic self-field, and survivability against debris itself; ii) assessing the dynamical relevance of tether parameters in implementing control laws to limit oscillations in /off the orbital plane, where passive stability may be marginal; iii) deriving a law for bare-tape current from numerical simulations and chamber tests, taking into account ambient magnetic field, ion ram motion, and adiabatic electron trapping; iv) determining requirements on a year-dormant hollow cathode under long times/broad emission-range operation, and trading-off against use of electron thermal emission; v) determining requirements on magnetic components and power semiconductors for a control module that faces high voltage/power operation under mass/volume limitations; vi) assessing strategies to passively deploy a wide conductive tape that needs no retrieval, while avoiding jamming and ending at minimum libration; vii) evaluating the tape structure as regards conductive and dielectric materials, both lengthwise and in its cross-section, in particular to prevent arcing in triple-point junctions.

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The interest in LED lighting has been growing recently due to the high efficacy, lifelime and ruggedness that this technology offers. However the key element to guarantee those parameters with these new electronic devices is to keep under control the working temperature of the semiconductor crystal. This paper propases a LED lamp design that fulfils the requ irements of a PV lighting systems, whose main quality criteria is reliability. It uses directly as a power supply a non·stabilized constant voltage source, as batteries. An electronic control architecture is used to regulate the current applied to the LEO matri)( according to their temperature and the voltage output value of the batteries with two pulse modulation signals (PWM) signals. The first one connects and disconnects the LEOs to the power supply and the second one connects and disconnects several emitters to the electric circuit changing its overall impedance. A prototype of the LEO lamp has been implemented and tested at different temperaturas and battery voltages.

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The performance efficiency of electrodynamic bare tethers acting as thrusters in low Earth orbit, as gauged by the ratio of the system mass dedicated to thrust over mission impulse, is analyzed and compared to the performance efficiency of electrical thrusters. Tether systems are much lighter for times beyond six months in space-tug operations, where there is a dedicated solar array, and beyond one month for reboost of the International Space Station, where the solar array is already in place. Bare-tether propulsive efficiency itself, with the tether considered as part of the power plant, is higher for space tugs. Tether optimization shows that thin tapes have greater propulsive efficiency and are less sensitive to plasma density variations in orbit than cylindrical tethers. The efficiency increases with tape length if some segment next to the power supply at the top is insulated to make the tether potential bias vanish at the lower end; multitape tethers must be used to keep the efficiency high at high thrust levels. The efficiency has a maximum for tether-hardware mass equal to the fraction of power-subsystem mass going into ohmic power, though the maximum is very flat. For space tugs, effects of induced-bias changes in orbit might need to be reduced by choosing a moderately large power-subsystem to tether-hardware mass ratio or by tracking the current-voltage characteristic of the solar array.

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The bandwidth achievable by using voltage mode control or current mode control in switch-mode power supply is limited by the switching frequency. Fast transient response requires high switching frequency, although lower switching frequencies could be more suitable for higher efficiency. This paper proposes the use of hysteretic control of the output capacitor $(C_{out})$ current to improve the dynamic response of the buck converter. An external voltage loop is required to accurately regulate the output voltage. The design of the hysteretic loop and the voltage loop are presented. Besides, it is presented a non-invasive current sensor that allows measuring the current in the capacitor. This strategy has been applied for DVS (dynamic voltage scaling) on a 5 MHz buck converter. Experimental results validate the proposed control technique and show fast transient response from 1.5 V to 2.5 V in 2 $mu{rm s}$.

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In high performance digital systems as well as in RF systems, voltage scaling and modulation techniques have been adopted to achieve a more efficient processing of the energy. The implementation of such techniques relies on a power supply that is capable of rapidly adjusting the system supply voltage. In this paper, a pulsewidth modulation multiphase topology with magnetic coupling is proposed for its use in voltage modulation techniques. Since the magnetic coupling in this topology is done with transformers instead of coupled inductors, the energy storage is reduced and very fast voltage changes are achieved. Advantages and drawbacks of this topology have been previously presented in the literature and in this paper, the design criteria for implementing a power supply for the envelope elimination and restoration technique in an RF system are presented along with an implementation of the power supply.

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Use of a (bare) conductive tape electrically floating in LEO as an effective e-beam source that produces artificial auroras, and is free of problems that have marred standard beams, is considered. Ambient ions impacting the tape with KeV energies over most of its length liberate secondary electrons, which race down the magnetic field and excite neutrals in the E-layer, resulting in auroral emissions. The tether would operate at night-time with both a power supply and a plasma contactor off; power and contactor would be on at daytime for reboost. The optimal tape thickness yielding a minimum mass for an autonomous system is determined; the alternative use of an electric thruster for day reboost, depending on mission duration, is discussed. Measurements of emission brightness from the spacecraft could allow determination of the (neutral) density vertical profile in the critical E-layer; the flux and energy in the beam, varying along the tether, allow imaging line-of-sight integrated emissions that mix effects with altitude-dependent neutral density and lead to a brightness peak in the beam footprint at the E-layer. Difficulties in tomographic inversion, to determine the density profile, result from beam broadening, due to elastic collisions, which flattens the peak, and to the highly nonlinear functional dependency of line-of-sight brightness. Some dynamical issues are discussed.