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Aircraft Flap Control System: Proposal of a Simulink Test Bench for Evaluating Innovative Asymmetry Monitoring and Control Techniques, file e384c42e-e579-d4b2-e053-9f05fe0a1d67
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885
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Modelling of a safety relief valve through a MATLAB-Simulink and CFD based approach, file e384c42f-4b02-d4b2-e053-9f05fe0a1d67
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719
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Reusable space tug concept and mission, file e384c42f-2ec3-d4b2-e053-9f05fe0a1d67
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513
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A methodology for innovative technologies roadmaps assessment to support strategic decisions for future space exploration., file e384c42e-2d82-d4b2-e053-9f05fe0a1d67
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477
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A new CFD-Simulink based systems engineering approach applied to the modelling of a hydraulic safety relief valve, file e384c42f-6737-d4b2-e053-9f05fe0a1d67
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424
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A New Prognostic Method Based on Simulated Annealing Algorithm to Deal with the Effects of Dry Friction on Electromechanical Actuators, file e384c42d-9353-d4b2-e053-9f05fe0a1d67
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308
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A methodology to support strategic decisions in future human space exploration: from scenario definition to building blocks assessment, file e384c42e-27f1-d4b2-e053-9f05fe0a1d67
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296
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Sensitivity Analysis for a PEM Fuel Cell Model aimed to Optimization, file e384c42d-763e-d4b2-e053-9f05fe0a1d67
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293
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Electromechanical actuators affected by multiple failures: a simulated-annealing-based fault identification algorithm, file e384c42e-e57b-d4b2-e053-9f05fe0a1d67
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274
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Linear Electromechanical Actuators Affected by Mechanical Backlash: a Fault Identification Method Based on Simulated Annealing Algorithm, file e384c42e-e577-d4b2-e053-9f05fe0a1d67
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261
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Risk Analysis of the Future Implementation of a
Safety Management System for Multiple RPAS Based
on First Demonstration Flights, file e384c42f-916c-d4b2-e053-9f05fe0a1d67
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249
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FUTURE SPACE EXPLORATION: FROM REFERENCE SCENARIO DEFINITION TO KEY TECHNOLOGIES ROADMAPS, file e384c42e-1c5e-d4b2-e053-9f05fe0a1d67
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242
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HUMAN EXPEDITION TO A NEAR EARTH ASTEROID: REFERENCE MISSION AND TECHNOLOGIES, file e384c42e-1e97-d4b2-e053-9f05fe0a1d67
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220
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Approximated models for aerodynamic coefficients estimation in a multidisciplinary design environment, file e384c42e-1752-d4b2-e053-9f05fe0a1d67
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188
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Proposal of Multidisciplinary Design Optimization Approach for a Proton Exchange Membrane Fuel Cell Performance Estimate, file e384c42e-e578-d4b2-e053-9f05fe0a1d67
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163
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Numerical modelling of sinusoidal brushless motor for aerospace actuator systems, file e384c42f-9505-d4b2-e053-9f05fe0a1d67
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155
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Design of the Environmental Control System of an Unmanned Aerial Vehicle through the MBSE, file e384c431-964e-d4b2-e053-9f05fe0a1d67
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154
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New Prognostic Method Based on Spectral Analysis Techniques Dealing with Motor Static Eccentricity for Aerospace Electromechanical Actuators, file e384c42d-75cd-d4b2-e053-9f05fe0a1d67
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148
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Application of dust removal technologies for future lunar exploration, file e384c42e-0659-d4b2-e053-9f05fe0a1d67
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137
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Electrohydraulic Servomechanisms Affected by Multiple Failures: A Model-Based Prognostic Method Using Genetic Algorithms, file e384c42f-2d66-d4b2-e053-9f05fe0a1d67
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137
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Electromechanical actuators affected by multiple failures: Prognostic method based on spectral analysis techniques, file e384c42f-885b-d4b2-e053-9f05fe0a1d67
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133
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A direct-drive solution for Hydrogen supplied all-electric airplane, file e384c42f-c9b1-d4b2-e053-9f05fe0a1d67
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133
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Multidisciplinary Integrated Framework for the Optimal Design of a Jet Aircraft Wing, file e384c42e-1cf6-d4b2-e053-9f05fe0a1d67
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130
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Robust simulation model approach to evaluate innovative asymmetry monitoring and control techniques in critical flap failure and aircraft controllability, file e384c42d-ac05-d4b2-e053-9f05fe0a1d67
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129
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Analysis of a Moon outpost for Mars enabling technologies through a Virtual Reality environment, file e384c42f-ddb3-d4b2-e053-9f05fe0a1d67
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116
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Proposal of a model based fault identification neural technique for more-electric aircraft flight control EM actuators, file e384c42e-e57a-d4b2-e053-9f05fe0a1d67
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92
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Proposal of a Fast Model-Based Prognostic Paradigm for Electrohydraulic Actuators affected by Multiple Failures, file e384c42f-4b01-d4b2-e053-9f05fe0a1d67
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82
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Development of a multifunctional panel for aerospace use through SLM Additive Manufacturing, file e384c431-cd5b-d4b2-e053-9f05fe0a1d67
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74
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Electromechanical Actuators Affected by Multiple Failures: Prognostic Method based on Wavelet Analysis Techniques, file e384c42f-9cb4-d4b2-e053-9f05fe0a1d67
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66
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Compression tests of ABS specimens for UAV components produced via the FDM technique, file e384c431-ebcd-d4b2-e053-9f05fe0a1d67
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65
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A Robust Multifunctional Sandwich Panel Design with Trabecular Structures by the Use of Additive Manufacturing Technology for a New De-Icing System, file e384c432-133c-d4b2-e053-9f05fe0a1d67
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62
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Special Issue on “Additive Manufacturing Technologies and Applications”, file e384c431-eaaa-d4b2-e053-9f05fe0a1d67
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55
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Permanent Magnet Synchronous Motor (PMSM) for Aerospace Servomechanisms: Proposal of a Lumped Model for Prognostics, file e384c431-3871-d4b2-e053-9f05fe0a1d67
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50
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Thermal condition monitoring of large smart bearing through fiber optic sensors, file e384c431-59b9-d4b2-e053-9f05fe0a1d67
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49
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Prognostics of onboard electromechanical actuators: A new approach based on spectral analysis techniques, file e384c430-4e8f-d4b2-e053-9f05fe0a1d67
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46
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Electrohydraulic actuators affected by multiple failures: Proposal of an alternative model-based prognostic paradigm, file e384c430-081b-d4b2-e053-9f05fe0a1d67
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44
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Evaluation of aiding and opposing load efficiency for an actuator planetary drive, file e384c432-b718-d4b2-e053-9f05fe0a1d67
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44
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3D FDM production and mechanical behavior of polymeric sandwich specimens embedding classical and honeycomb cores., file e384c431-2637-d4b2-e053-9f05fe0a1d67
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41
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Preliminary Analysis on Environmental and Intrinsic Factors on FBG-Based Vibration Sensors, file e384c434-afad-d4b2-e053-9f05fe0a1d67
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37
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Model-Based Fault Detection and Identification for Prognostics of Electromechanical Actuators Using Genetic Algorithms, file e384c431-09e8-d4b2-e053-9f05fe0a1d67
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34
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Design and Development of a Planetary Gearbox for Electromechanical Actuator Test Bench through Additive Manufacturing, file e384c432-19df-d4b2-e053-9f05fe0a1d67
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34
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Multifidelity domain-aware learning for the design of re-entry vehicles, file e384c434-3ff7-d4b2-e053-9f05fe0a1d67
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34
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Design and development of innovative FBG-based fiber optic sensors for aerospace applications, file e384c432-67f7-d4b2-e053-9f05fe0a1d67
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33
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Sandwich panel with lattice core for aircraft anti-ice system made by Selective Laser Melting, file e384c430-161e-d4b2-e053-9f05fe0a1d67
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32
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Experimental comparison of Fiber Bragg Grating installation techniques for aerospace systems, file e384c431-3875-d4b2-e053-9f05fe0a1d67
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31
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Design and Development of an Electromechanical Actuator Test Bench for Validation of Health Monitoring Models, file e384c434-710d-d4b2-e053-9f05fe0a1d67
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28
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Feasibility study of FBG-based sensors for prognostics in aerospace applications, file e384c430-dd3e-d4b2-e053-9f05fe0a1d67
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27
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Power generation system for l-moxie: Concept proposal and trade-off analysis, file e384c434-b4f3-d4b2-e053-9f05fe0a1d67
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27
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The thermal control system of NASA’s Curiosity rover: a case study, file e384c434-8c7e-d4b2-e053-9f05fe0a1d67
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24
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Proposal of prognostic parametric method applied to an electrohydraulic servomechanism affected by multiple failures, file e384c42e-37db-d4b2-e053-9f05fe0a1d67
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23
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A simplified monitor model for EMA prognostics, file e384c430-7d3a-d4b2-e053-9f05fe0a1d67
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23
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A simplified monitoring model for PMSM servoactuator prognostics, file e384c431-3022-d4b2-e053-9f05fe0a1d67
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22
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Simplified models for mechanical transmission efficiency with opposing and aiding loads, file e384c431-36ad-d4b2-e053-9f05fe0a1d67
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22
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Additive Manufacturing Technologies and Applications, file e384c431-ef1c-d4b2-e053-9f05fe0a1d67
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22
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Prognostics of onboard electrohydraulic servomechanisms: Proposal of a novel model-based fault detection neural technique, file e384c430-0174-d4b2-e053-9f05fe0a1d67
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21
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Study of Packaging and Installation of FBG Sensors for Monitoring of Aircraft Systems, file e384c432-e06b-d4b2-e053-9f05fe0a1d67
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21
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PROGNOSTICS OF AEROSPACE ELECTROMECHANICAL ACTUATORS USING THE FAILURE MAPS TECHNIQUE, file b911ad8c-bbc7-4d9f-942b-51c2f27f63e1
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20
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Evaluations on adequacy and utility of Failure Modes and Effects and Criticality Analysis and Fault Tree Analysis methodologies applied to civil RPAS systems, file e384c430-6094-d4b2-e053-9f05fe0a1d67
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19
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Fault Detection and Identification Method Based on Genetic Algorithms to Monitor Degradation of Electrohydraulic Servomechanisms, file e384c432-9502-d4b2-e053-9f05fe0a1d67
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19
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A New Method for Friction Estimation in EMA Transmissions, file e384c433-f6ca-d4b2-e053-9f05fe0a1d67
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18
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Innovative actuator fault identification based on back electromotive force reconstruction, file e384c432-2ee2-d4b2-e053-9f05fe0a1d67
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17
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Actuator Load Estimation From Distributed Optical Sensing of Airframe Deformation, file e384c434-99be-d4b2-e053-9f05fe0a1d67
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17
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New prognostic neural method by discrete wavelet transforms for electromechanical flight controls affected by progressive faults, file e384c430-7cde-d4b2-e053-9f05fe0a1d67
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16
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A simplified monitoring model for PMSM servoactuator prognostics, file e384c431-3023-d4b2-e053-9f05fe0a1d67
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16
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Characterization of ABS specimens produced via the 3D printing technology for drone structural components, file e384c432-0177-d4b2-e053-9f05fe0a1d67
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16
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Evaluations on hydrogen fuel cells as a source of energy
for specific operations category civil RPAS systems, file e384c430-41ca-d4b2-e053-9f05fe0a1d67
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15
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Fiber Bragg Gratings for Prognostics in Space Applications: A Thermo-Mechanical Characterization of Minimally Invasive Sensing Techniques, file e384c433-d2a3-d4b2-e053-9f05fe0a1d67
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15
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A new genetic algorithm model-based prognostic approach applied to onboard electrohydraulic servomechanisms, file e384c430-081a-d4b2-e053-9f05fe0a1d67
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14
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Model based analysis of precursors of electromechanical servomechanisms failures using an artificial neural network, file e384c42e-36e6-d4b2-e053-9f05fe0a1d67
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13
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Failure Modes and Effects and Criticality Analysis and Fault Tree Analysis methodologies applied to civil RPAS systems, file e384c430-6093-d4b2-e053-9f05fe0a1d67
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13
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A first-order lumped parameters model of electrohydraulic actuators for low-inertia rotating systems with dry friction, file e384c432-b1e0-d4b2-e053-9f05fe0a1d67
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13
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Optical fibers applied to aerospace systems prognostics: Design and development of new FBG-based vibration sensors, file e384c433-ef02-d4b2-e053-9f05fe0a1d67
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13
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Experimental comparison of Fiber Bragg Grating installation techniques for aerospace systems, file e384c431-3874-d4b2-e053-9f05fe0a1d67
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12
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A sensor fusion strategy based on a distributed optical sensing of airframe deformation applied to actuator load estimation, file e384c433-b02f-d4b2-e053-9f05fe0a1d67
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12
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Model-based strategy and surrogate function for health condition assessment of actuation devices, file e384c433-d4b3-d4b2-e053-9f05fe0a1d67
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12
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Diagnostics of electro-mechanical actuators based upon the back-EMF reconstruction, file e384c433-e636-d4b2-e053-9f05fe0a1d67
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12
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Thermal condition monitoring of large smart bearing through fiber optic sensors, file e384c430-d1de-d4b2-e053-9f05fe0a1d67
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11
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Additive Manufacturing Evaluation Tool for Design Studies, file e384c431-2638-d4b2-e053-9f05fe0a1d67
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11
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Electromechanical servomechanisms affected by motor static eccentricity: Proposal of fault evaluation algorithm based on spectral analysis techniques, file e384c42e-f048-d4b2-e053-9f05fe0a1d67
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9
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An Improved Fault Identification Method for Electromechanical Actuators, file e384c434-d419-d4b2-e053-9f05fe0a1d67
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9
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Prognostics of onboard electrohydraulic servomechanisms: Proposal of a novel model-based fault detection neural technique, file e384c430-01b4-d4b2-e053-9f05fe0a1d67
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8
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Study of FBG-based optical sensors for thermal measurements in aerospace applications, file d5992ca1-d328-434e-b244-e0637157ae0b
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6
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High gear ratio mechanical transmissions for actuators: Simplified models for efficiency under opposing and aiding loads, file e384c433-fd40-d4b2-e053-9f05fe0a1d67
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6
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Permanent Magnet Synchronous Motor (PMSM) for Aerospace Servomechanisms: Proposal of a Lumped Model for Prognostics, file e384c431-3870-d4b2-e053-9f05fe0a1d67
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5
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Specific Category Operations Within the U-Space: Expert Systems Embedded Within RPAS as an Original Mean of Mitigation of Operational Safety Risks, file e384c433-fdf9-d4b2-e053-9f05fe0a1d67
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5
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Innovative sensor networks for massive distributed thermal measurements in space applications under different environmental testing conditions, file 66dc4613-c421-4e4e-b7e8-9b5715208797
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4
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Air-To-Ground Transmission and Near Real-Time Visualization of FBG Sensor Data Via Cloud Database, file b626f32f-8aa9-46ac-850c-cac45928041f
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4
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Evaluation of the correlation coefficient as a prognostic indicator for electromechanical servomechanism failures, file e384c42d-e2b6-d4b2-e053-9f05fe0a1d67
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4
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Human life support in permanent lunar base architectures, file e384c42e-328d-d4b2-e053-9f05fe0a1d67
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4
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A Virtual Reality approach for studying a future human lunar outpost: an integrated simulation case study of a Stand Alone Power System, file e384c42f-c0b7-d4b2-e053-9f05fe0a1d67
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4
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Lattice structured impact absorber with embedded anti-icing system for aircraft wings fabricated with additive SLM process, file e384c431-5c86-d4b2-e053-9f05fe0a1d67
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4
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Specific Category Operations Within the U-Space: Expert Systems Embedded Within RPAS as an Original Mean of Mitigation of Operational Safety Risks, file e384c433-be1e-d4b2-e053-9f05fe0a1d67
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4
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LuNaDrone: Small Autonomous Spacecraft for Lunar Lava Tubes Exploration, file cc08e9ba-5da8-4c50-858c-b91415441412
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3
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Incremental architectures for a permanent human lunar outpost with focus on isru technologies., file e384c42e-328e-d4b2-e053-9f05fe0a1d67
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3
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Development of an Environmental Control System Pack simulation model for a More Electric Aircraft, file e384c42e-3614-d4b2-e053-9f05fe0a1d67
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3
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A novel design approach for space components: application to a multifunctional panel, file e384c42f-c0b8-d4b2-e053-9f05fe0a1d67
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3
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Virtual Reality to assist the engineering decision-making process: improving the Concurrent Design approach, file e384c42f-c361-d4b2-e053-9f05fe0a1d67
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3
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A Lumped Parameter High Fidelity EMA Model for Model-Based Prognostics, file e384c431-353c-d4b2-e053-9f05fe0a1d67
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3
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Characterization of ABS specimens produced via the 3D printing technology for drone structural components, file e384c431-ec1d-d4b2-e053-9f05fe0a1d67
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3
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Back-EMF Reconstruction for Electromechanical Actuators in Presence of Faults, file e384c432-da1c-d4b2-e053-9f05fe0a1d67
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3
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| Totale |
8573 |
Archivio Istituzionale della Ricerca