Electro-Mechanical Actuators for Safety-Critical Aerospace Applications
Aircraft electrification is one of the most important and strategic initiatives currently supporting the innovation of the aviation industry. This manifests in the well-known more-electric aircraft concept (with the ultimate aim of achieving the all-electric long-term target), which aims to graduall...
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Format: | Electronic Book Chapter |
Language: | English |
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Basel
MDPI - Multidisciplinary Digital Publishing Institute
2023
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Online Access: | DOAB: download the publication DOAB: description of the publication |
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100 | 1 | |a Di Rito, Gianpietro |4 edt | |
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245 | 1 | 0 | |a Electro-Mechanical Actuators for Safety-Critical Aerospace Applications |
260 | |a Basel |b MDPI - Multidisciplinary Digital Publishing Institute |c 2023 | ||
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520 | |a Aircraft electrification is one of the most important and strategic initiatives currently supporting the innovation of the aviation industry. This manifests in the well-known more-electric aircraft concept (with the ultimate aim of achieving the all-electric long-term target), which aims to gradually replace onboard systems based on mechanical, hydraulic, or pneumatic power sources with electrically powered ones to reduce the weight and costs, optimize energy, and increase the eco-compatibility and reliability of future aircrafts.A key technological enabler for pursuing these challenging objectives is electro-mechanical actuation. The applicability of electro-mechanical actuators (EMAs) in aerospace has been proved in terms of dynamic performances, but it still entails several concerns in terms of reliability/safety and operation in a harsh environment. In civil aircrafts, EMAs are often avoided for safety-critical functions (flight controls, brakes, landing gears, and nose wheel steering), essentially because the statistical database on the components' fault modes is poor.This Special Issue is thus focused on advancements and innovations in the design, modelling/simulation, architectural definition, reliability/safety analysis, control, condition-monitoring, and experimental testing of EMAs developed for safety-critical aerospace applications. The research papers included in this Special Issue will undoubtedly contribute to progress towards the objective of more electric flights. | ||
540 | |a Creative Commons |f https://creativecommons.org/licenses/by/4.0/ |2 cc |4 https://creativecommons.org/licenses/by/4.0/ | ||
546 | |a English | ||
650 | 7 | |a Technology: general issues |2 bicssc | |
650 | 7 | |a History of engineering & technology |2 bicssc | |
653 | |a more electric vehicles | ||
653 | |a dissimilar redundant actuation system | ||
653 | |a NSGA-II algorithm | ||
653 | |a optimization design | ||
653 | |a electrically actuated nose wheel steering | ||
653 | |a all-electric aircraft | ||
653 | |a electromagnetic damper | ||
653 | |a electromagnetic simulation | ||
653 | |a landing gear shimmy reduction | ||
653 | |a shape control | ||
653 | |a macro-fiber composites | ||
653 | |a bending | ||
653 | |a twisting | ||
653 | |a experimental validation | ||
653 | |a control system | ||
653 | |a actuator | ||
653 | |a aerospace | ||
653 | |a electromechanical | ||
653 | |a flight control | ||
653 | |a friction | ||
653 | |a modelling | ||
653 | |a position control | ||
653 | |a preliminary design | ||
653 | |a simulation | ||
653 | |a validation | ||
653 | |a fixed-wing UAV | ||
653 | |a full-electric propulsion system | ||
653 | |a axial-flux PMSMS | ||
653 | |a fault-tolerant control | ||
653 | |a phase-to-ground short circuit | ||
653 | |a failure transient analysis | ||
653 | |a prognostics | ||
653 | |a electromechanical actuators | ||
653 | |a neural network | ||
653 | |a temperature | ||
653 | |a all-electric propulsion | ||
653 | |a electric machines | ||
653 | |a fault diagnosis | ||
653 | |a inter-turn short circuit | ||
653 | |a specification | ||
653 | |a flight analysis | ||
653 | |a dimensional analysis | ||
653 | |a vibration | ||
653 | |a multidisciplinary optimization | ||
653 | |a health monitoring | ||
653 | |a electro-mechanical actuators | ||
653 | |a testing | ||
653 | |a reliability | ||
653 | |a fault-tolerant systems | ||
653 | |a aircraft anti-skid braking system | ||
653 | |a actuator faults | ||
653 | |a reconfiguration control | ||
653 | |a linear active-disturbance rejection control | ||
653 | |a deep reinforcement learning | ||
653 | |a twin delayed deep deterministic policy gradient algorithm | ||
653 | |a active cylindrical coupler | ||
653 | |a correction coefficient | ||
653 | |a finite element method | ||
653 | |a hybrid UAV | ||
653 | |a magnetic coupler | ||
653 | |a magnetic coupling | ||
653 | |a noncontact torque transmission | ||
653 | |a mean magnetic field | ||
653 | |a wire diameter | ||
653 | |a coil | ||
653 | |a sinusoidal response | ||
653 | |a square-wave response | ||
653 | |a incremental nonlinear dynamic inversion (INDI) | ||
653 | |a actuator compensation | ||
653 | |a model reduction | ||
653 | |a pseudo-control hedging (PCH) | ||
653 | |a helicopter attitude control | ||
856 | 4 | 0 | |a www.oapen.org |u https://mdpi.com/books/pdfview/book/7442 |7 0 |z DOAB: download the publication |
856 | 4 | 0 | |a www.oapen.org |u https://directory.doabooks.org/handle/20.500.12854/101347 |7 0 |z DOAB: description of the publication |