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Control of Aircraft Electrical Power System

A special issue of Energies (ISSN 1996-1073). This special issue belongs to the section "A: Sustainable Energy".

Deadline for manuscript submissions: closed (10 December 2020) | Viewed by 3584

Special Issue Editor


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Guest Editor
Power Electronics, Machines, and Control Group (PEMC), University of Nottingham, Nottingham NG7 2RD, UK
Interests: electrical power systems; control; stability; power generation; power quality; power management and distribution; optimization; advanced modelling; simulation methods
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Special Issue Information

Dear Colleagues,

Transportation electrification is considered as one of the key approaches to address global environmental concerns and to achieve sustainable future. In the aviation sector, long-term roadmap ACARE Flightpath 2050 targets a 75% reduction of CO2 and 90% of NOX emissions per passenger per kilometre. Achieving these challenging goals requires reconsideration of the underlying concepts of future aircraft. Many new aircraft types are now being developed, spanning from small drones and urban air vehicles to large passenger aircrafts. All these significantly rely on green electric energy, from adopting new electrically-driven secondary onboard systems to hybrid-electric and fully-electric primary propulsive systems. As such, onboard electric power systems (EPS) need to adopt these changes and become the backbone of future electrified aircraft. Therefore, it is essential to establish routes towards safe, reliable and highly efficient airborne EPS operation.

This Special Issue will address control challenges in future aircraft EPS, and papers investigating innovations is this area are invited. Topics may include but not be limited to EPS global and local control strategies, architectural solutions, power and energy management and optimisation, power routing and reconfiguration, electric power quality and stability issues.

Prof. Serhiy Bozhko
Guest Editor

Manuscript Submission Information

Manuscripts should be submitted online at www.mdpi.com by registering and logging in to this website. Once you are registered, click here to go to the submission form. Manuscripts can be submitted until the deadline. All submissions that pass pre-check are peer-reviewed. Accepted papers will be published continuously in the journal (as soon as accepted) and will be listed together on the special issue website. Research articles, review articles as well as short communications are invited. For planned papers, a title and short abstract (about 100 words) can be sent to the Editorial Office for announcement on this website.

Submitted manuscripts should not have been published previously, nor be under consideration for publication elsewhere (except conference proceedings papers). All manuscripts are thoroughly refereed through a single-blind peer-review process. A guide for authors and other relevant information for submission of manuscripts is available on the Instructions for Authors page. Energies is an international peer-reviewed open access semimonthly journal published by MDPI.

Please visit the Instructions for Authors page before submitting a manuscript. The Article Processing Charge (APC) for publication in this open access journal is 2600 CHF (Swiss Francs). Submitted papers should be well formatted and use good English. Authors may use MDPI's English editing service prior to publication or during author revisions.

Keywords

  • electric power system
  • aircraft
  • control
  • architecture
  • energy management
  • power quality
  • stability

Published Papers (1 paper)

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Research

17 pages, 7339 KiB  
Article
Assessment of Training Aircraft Crew Exposure to Electromagnetic Fields Caused by Radio Navigation Devices
by Joanna Michałowska, Jarosław Pytka, Arkadiusz Tofil, Piotr Krupski and Łukasz Puzio
Energies 2021, 14(1), 254; https://doi.org/10.3390/en14010254 - 05 Jan 2021
Cited by 8 | Viewed by 3098
Abstract
The paper depicts research concerning the value of the electric component of the electromagnetic (EM) energy determined by the NHT3DL meter by Microrad with the 01E measuring probe during a number of flights made by Aero AT-3 R100, Cessna C172, and Tecnam P2006T [...] Read more.
The paper depicts research concerning the value of the electric component of the electromagnetic (EM) energy determined by the NHT3DL meter by Microrad with the 01E measuring probe during a number of flights made by Aero AT-3 R100, Cessna C172, and Tecnam P2006T fixed wing aircrafts and a Robinson R44 Raven helicopter. The point of reference for the recorded measurement was the normative limits of the electromagnetic field (EMF), which can influence a pilot in the course of a flight. Selected studies of the maximum value recorded by the meter was E = 10.66 V/m when landing at an airfield equipped with the VHF (Very High Frequency) omnidirectional radio range (VOR) approach system. Particular attention has been paid to changes in electric field intensity during the operation and their effects on the type of radio navigation systems as well as communication with the airfield control tower. The obtained results were validated in the Statistica 13.3 software for the purpose of a detailed stochastic analysis of the tested values. Results obtained are subject to the mandatory requirements of Directive 2013/35/EU as well as to the relevant regulations in Poland. Full article
(This article belongs to the Special Issue Control of Aircraft Electrical Power System)
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