Alessandra Menicucci

ORCID: 0000-0002-7064-6275
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About
Contact & Profiles
Research Areas
  • Radiation Effects in Electronics
  • Spacecraft Design and Technology
  • Astro and Planetary Science
  • Radiation Therapy and Dosimetry
  • Particle Detector Development and Performance
  • Planetary Science and Exploration
  • Dark Matter and Cosmic Phenomena
  • Satellite Communication Systems
  • Particle physics theoretical and experimental studies
  • Space Satellite Systems and Control
  • Radiation Detection and Scintillator Technologies
  • Solar and Space Plasma Dynamics
  • Space Exploration and Technology
  • Parallel Computing and Optimization Techniques
  • Embedded Systems Design Techniques
  • VLSI and Analog Circuit Testing
  • Quantum Chromodynamics and Particle Interactions
  • Integrated Circuits and Semiconductor Failure Analysis
  • Advanced Battery Technologies Research
  • Spacecraft and Cryogenic Technologies
  • Real-Time Systems Scheduling
  • Semiconductor materials and devices
  • High-Energy Particle Collisions Research
  • Inertial Sensor and Navigation
  • Neutrino Physics Research

Delft University of Technology
2016-2024

Jet Propulsion Laboratory
2023

European Space Research and Technology Centre
2011-2022

Oceaneering International (United States)
2016-2021

Innovative Solution In Space (Netherlands)
2021

University of Rome Tor Vergata
2004-2005

Istituto Nazionale di Fisica Nucleare, Sezione di Roma I
2003

Sapienza University of Rome
2002

The objective of this paper is to investigate which approach would lead more reliable CubeSats: full subsystem redundancy or improved testing. Based on data from surveys, the reliability satellites and subsystems estimated using a Kaplan–Meier estimator. Subsequently, variety models defined their maximum likelihood estimates are compared. A product Lognormal distribution addressing immaturity failure Gompertz wear-out found best represent CubeSat reliability. Bayesian inference used find...

10.1016/j.ress.2021.108288 article EN cc-by Reliability Engineering & System Safety 2022-01-08

The Earth-Moon system is constantly bombarded by meteoroids of different size and impact speed. Observation the impacts on Moon can enable thorough characterization Lunar meteoroid flux, which similar to that Earth. While Earth-based observations are restricted weather, geometric illumination conditions, a Lunar-based observation campaign improve detection rate and, when observing far side, complement in both space time taken from Meteoroid Impact Observer (LUMIO), one two winning concepts...

10.1016/j.actaastro.2022.03.032 article EN cc-by-nc-nd Acta Astronautica 2022-03-26

The estimation of the relative pose an inactive spacecraft by active servicer is a critical task for close-proximity operations, such as In-Orbit Servicing and Active Debris Removal. Among all challenges, lack available space images satellite makes on-ground validation current monocular camera-based navigation systems challenging task, mostly due to fact that standard Image Processing (IP) algorithms, which are usually tested on synthetic images, tend fail when implemented in orbit. In...

10.1016/j.actaastro.2022.04.002 article EN cc-by Acta Astronautica 2022-04-10

The solar energetic particle (SEP) radiation environment is an important consideration for spacecraft design, mission planning and human spaceflight. Herein presented investigation into the likely severity of effects a very large Solar Particle Event (SPE) on technology humans in space. Fluences SPEs derived using statistical models are compared to historical verify their appropriateness use analysis which follows. By combining tools with model behind varying layers shielding it possible...

10.1051/swsc/2014017 article EN cc-by Journal of Space Weather and Space Climate 2014-01-01

This paper proposes a roadmap to address present and future needs in space systems with RISC-V processors. is an open modular instruction set architecture, which rapidly growing popularity terrestrial applications. To satisfy different applications contrasting requirements satellite data systems, four types of processors are identified: 1) low-area/low-power microcontrollers, 2) on-board computers, 3) general-purpose for payloads, 4) enhanced payload artificial intelligence. Several...

10.2514/1.i010735 article EN Journal of Aerospace Information Systems 2019-08-05

The effects of heavy-ion test conditions and beam energy on device response are investigated. These illustrated with two types vehicles: SRAMs power MOSFETs. In addition, GEANT4 simulations have also been performed to better understand the results. Testing high fluence levels is required detect rare events. This increases probability nuclear interactions. typically case for MOSFETs, which tested at fluences single event burnout or gate rupture detection, single-event-upset (SEU) measurement...

10.1109/tns.2012.2187681 article EN IEEE Transactions on Nuclear Science 2012-04-05

The roadmap for space exploration foresees longer journeys and further excursions outside low-Earth orbit as well the establishment of permanent outposts on other celestial bodies, such Moon or Mars. design spacecrafts habitats depends heavily mission scenario must consider radiation protection properties structural components dedicated shielding. In fact, short- long-term effects caused by exposure to cosmic are now considered among main health risks travel. One current strategies is find...

10.1667/rr15111.1 article EN Radiation Research 2018-08-20

The effects of heavy-ion test conditions and beam energy on device response are investigated. These illustrated with two types vehicles; SRAMs power MOSFETs. In addition, GEANT4 simulations have also been performed to better understand the results.

10.1109/radecs.2011.6131365 article EN 2011-09-01

Several Research and Development activities are ongoing at European Space Agency [1] to secure the supply of key electronic parts for current future space avionics systems. Analogously astro-particle high-energy physics, missions radiation environment drives hardness requirements, which limits availability suitable components. In particular ESA flagship Jupiter science mission, necessary processing, reliability, mass, power performance requirements difficult meet with components systems...

10.1088/1748-0221/8/02/c02007 article EN Journal of Instrumentation 2013-02-04

RISC-V is an open and modular Instruction Set Architecture(ISA) which rapidly growing in popularity terrestrial applications. This paper presents the place future space embedded systems ESA's roadmap for based processors. In order to satisfy different applications with contrasting requirements satellite data systems, four types of processors are identified: 1) General-Purpose (GP) payloads 2) main platform On-Board Computers (OBCs) controllers 3) low-area/low-power microcontrollers (uCs), 4)...

10.1109/aero53065.2022.9843361 article EN 2022 IEEE Aerospace Conference (AERO) 2022-03-05

The ESA SEU-Monitor, a 2 Gbit DDR2 SDRAM and 100 V n-channel power MOSFET have been irradiated at GSI with ions of energies from 80 to 1500 MeV/n. measured SEE sensitivities are compared low energy <formula formulatype="inline" xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink"> <tex Notation="TeX">$(&lt;50\ {\rm MeV/n})$</tex></formula> data. SEU-Monitor the showed only differences in cross sections below ionization threshold. Here were lower for high...

10.1109/tns.2012.2201502 article EN IEEE Transactions on Nuclear Science 2012-07-10

This study focuses on the ion species and energy dependence of heavy SEE cross section in sub-LET threshold region through a set experimental data. In addition, Monte Carlo based model is introduced applied, showing good agreement with data several hundred MeV/n range while evidencing large discrepancies measurements 10-30 interval, notably for Ne ion. Such are carefully analyzed discussed.

10.1109/tns.2015.2483021 article EN IEEE Transactions on Nuclear Science 2015-12-01

The use of deep neural networks (DNNs) in terrestrial applications went from niche to widespread a few years, thanks relatively inexpensive hardware for both training and inference, large datasets available. applicability this paradigm space systems, where are not readily available, is more difficult thus still rare. This paper analyzes the impact DNNs on system-level capabilities systems terms on-board decision making (OBDM) identifies specific criticalities deploying satellites. workload...

10.2514/1.i010916 article EN Journal of Aerospace Information Systems 2021-06-28

This paper discusses principles and techniques to evaluate processors for dependable computing in space applications. The focus is on soft errors, which dominate the failure rate of space. Error, propagation models from literature are selected employed estimate due errors typical processor designs. A similar approach can be followed applications with different radiation environments (e.g. automotive, servers, experimental instrumentation exposed ground), by adapting error models. detailed...

10.1016/j.cosrev.2020.100349 article EN cc-by Computer Science Review 2020-12-24

Abstract PocketQubes are a form factor of highly miniaturized satellites with body one or more cubic units 5 cm. In this paper, the characteristics in terms their constraints and (potential) utility treated. To avoid space debris limit collision risk, orbits need to be constraint. An analysis orbital decay has been carried out which, considering existing regulations pro-active attitude, should preferably launched low Earth below 400 km altitude. Due technical constraints, such as factor,...

10.1007/s12567-020-00300-0 article EN cc-by CEAS Space Journal 2020-02-05

This paper introduces an adaptive Convolutional Neural Network (CNN)-based Unscented Kalman Filter for the pose estimation of uncooperative spacecraft. The validation is carried out at Stanford's robotic Testbed Rendezvous and Optical Navigation on Satellite Hardware-In-the-loop Trajectories (SHIRT) dataset, which simulates vision-based rendezvous trajectories a servicer spacecraft to PRISMA's Tango proposed navigation system stress-tested synthetic as well realistic lab imagery by...

10.1016/j.asr.2023.02.021 article EN cc-by Advances in Space Research 2023-03-18

The use of System-on-Chip (SoC) solutions in the design on-board data handling systems is an important step towards further miniaturization space. However, Total Ionizing Dose (TID) and Single Event Effects (SEE) characterization these complex devices present new challenges that are either not fully addressed by current testing guidelines or may result expensive, cumbersome test configurations. In this paper we report setups, procedures results for TID a SoC microcontroller both using...

10.1016/j.net.2018.07.010 article EN cc-by-nc-nd Nuclear Engineering and Technology 2018-07-20

This paper discusses radiation tests on complex System-on-Chip (SoC) controllers using Low-Energy Protons (LEPs). The aim of this novel set guidelines is to be also applicable System In Package (SIP) or hybrid components that are now often used overcome printed circuit board's real estate restrictions in Hi-Rel electronics. Despite the growing success microcontrollers SoC HiRel applications, general and standardized methods for Single Event Effects (SEE) testing SoCs have not been widely...

10.1109/dft.2016.7684084 article EN 2016-09-01
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