Luigi Schirone
Sapienza University of Rome
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Publication
Featured researches published by Luigi Schirone.
IEEE Transactions on Industrial Electronics | 2014
Luigi Schirone; Michele Macellari
Power losses in high-efficiency dc-dc step up converters based on the synchronous three-level neutral-point-clamped (TLNPC) configuration were investigated. TLNPC converters benefit from the reduced stress on components and from the noninsulated stacked-boost output stage to provide reduced power losses and large voltage gains. Several prototypes with increasing efficiency were produced and tested; voltage gains larger than 20× were achieved by means of hard-switched prototypes with composite switches consisting of both low-Rds(ON) and highspeed MOSFETs. At lower voltage gains conversion efficiencies exceeding 98% were demonstrated. A thorough loss analysis is reported, extended to subtle power dissipation processes, which in high efficiency converters grow in relevance after weakening of the major loss mechanisms. The related model is proven capable to accurately predict circuit performance in a wide range of operating conditions.
international conference on environment and electrical engineering | 2015
Mauro Feliziani; Tommaso Campi; Silvano Cruciani; Francesca Maradei; Umberto Grasselli; M. Macellari; Luigi Schirone
The paper provides an investigation of a possible application of wireless power transfer (WPT) technology to recharge the battery of a short-distance electric vehicle. The performance of the WPT system working at 85 kHz is first investigated by simulations. A robust LCC compensation network suitably tuned is then investigated with the goal to analyze the influence of design parameters on the compensation strategy. Particular attention is addressed to evaluate the deterioration of the WPT system performance due to coil misalignment. Finally, the WPT performances are evaluated demonstrating the feasibility of the proposed WPT technology.
ieee international conference on renewable energy research and applications | 2015
Luigi Schirone; Michele Macellari
Several issues related to the prospected fast growth of the circulating Electric Vehicles are analysed. The environmental and economical topics are investigated first. Then several approaches for on-board charge management are reviewed and compared on the basis of efficiency, environmental impact and charging time. A particular effort is devoted to stress the potential benefits and limitations of Battery Swapping, and to outline the upgrades of Electric Vehicle design required to enable and promote its diffusion.
ieee international electric vehicle conference | 2014
Michele Macellari; Fabio Celani; Luigi Schirone
An analog dynamic dead time generator for synchronous boost converters based on GaN transistors is presented. A prototype was designed to operate at switching frequencies in the MHz range, with wide variations of the output voltage, and experimentally demonstrated its capability to stabilize the dead time duration to a few nanoseconds, independent of wide variations of the switching times of the transistor in use.
ieee aerospace conference | 2015
Michele Macellari; Giovanni B. Palmerini; Luigi Schirone
This work deals with the Electrical Power System of the Lunar Rover, developed for the AMALIA mission, intended to compete in the Google Lunar X prize. The main subsystems are described and their operation analyzed on the basis of the observed experimental behavior. Primary generation is provided by triple-junction solar cells, arranged as four sections, each connected to a dedicated Array Power Regulator with separate Maximum Power Point Tracking. A Switch Matrix allows to rearrange the inter-connections among the Solar Array sections and the APR in order to manage possible failures. During load peaks and/or with low Sun elevation the solar array is supported by a secondary generator consisting of three redundant units with Li-Ion battery cells. Two alternate configurations of the Battery Subsystem were developed: a classical 8S Li-Ion battery, for a 28V Sun-regulated bus, and a novel approach, based on a single-cell (1S) Li-Ion battery and a high-voltage-gain Battery Charge-Discharge Regulator. A specific converter was designed for this configuration, based on the non-insulated Three Levels Neutral Point Clamped switching converter topology. Its correct operation with bus voltages up to 48V and fully discharged battery cells was demonstrated.
conference of the industrial electronics society | 2013
Michele Macellari; Luigi Schirone
High-efficiency dc-dc step up converters, based on the synchronous Three Levels Neutral Point Clamped configuration were built and investigated. The baseline circuit based on hard-switched, fast high-current MOSFETs provided high efficiency levels on a wide range of operating conditions. Several approaches to further improve performance were investigated. Very high efficiencies were experimentally demonstrated by an hard switched configuration where the switches consisted of a suitable arrangement of very-low RDSon and very fast MOSFET transistors.
ieee aerospace conference | 2012
Michele Macellari; Giovanni B. Palmerini; Luigi Schirone
A Battery Charge-Discharge regulator (BCDR) intended to interface a 12V bus with a single-cell Li-ion battery for power levels in the 100W range is presented. It may be useful in small space vehicles, and especially in the cases when battery sizing is driven by the need to complement the power provided by primary power sources during high peaks of load, with comparatively small energy amounts. In particular, the Bidirectional Three Level Neutral Point Clamped (TLNPC) converter configuration was selected, and a prototype was designed, built and tested. After providing a rationale of the single-battery-cell approach, and of the criteria adopted to select the TLNPC converter circuit, the paper reports the principles of operation of the converter and indicates the design criteria for the main circuit parameters. Extensive characterization of the prototype completes the work.
Sustainability | 2017
Luigi Schirone; Filippo Pellitteri
Sustainability of current energy policies and their mid-term outlooks are investigated. First, an overview is given about the trend of global energy demand and energy production. The share of energy sources and the geographic distribution of demand are analysed on the basis of the statistics and projections published by major agencies. Sustainability of selected renewable energy sources is then explored. Finally, potential use of Hydrogen for energy storage in systems with high share of renewable sources is investigated.
ieee aerospace conference | 2009
Luigi Schirone; Michele Macellari; Alfiero Schiaratura
Modular power conversion systems for space application, thanks to their flexibility, can be easily adapted with minor changes to missions with different power requirements. In the perspective of an application to low-cost satellite, based on Commercial Off The Shelf components, the main design drivers are efficiency and reliability. We will focus our attention to spacecrafts with body-mounted solar cells. Thus, trade-off between the opposite requirements, efficiency and reliability, have been discussed through the analysis of several redundancy schemes. Reliability calculation of circuits will be performed on the basis of MIL-HDBK-217F. The aim of this work is to demonstrate that specific design efforts allow to increase the reliability of COTS-based power systems to levels comparable to classical systems based on spacequalified components.
ieee aerospace conference | 2006
Michele Macellari; R. Russo; Luigi Schirone
A special architecture for photovoltaic generation of electricity has been studied for a mission to Mercury. This paper deals with solar panel design primary concerns, with regards to the harsh Hermian thermal environment and to the need for great amounts of power for solar electric propulsion at 1 A.U.. A novel concept of a combined system of photovoltaic generators together with Fresnel lens solar concentrators will be presented as a possible solution to the different power demands of the whole mission