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Advances in Flight Dynamics and Autonomous Control of UAVs

A special issue of Applied Sciences (ISSN 2076-3417). This special issue belongs to the section "Aerospace Science and Engineering".

Deadline for manuscript submissions: closed (31 January 2023) | Viewed by 4918

Special Issue Editor


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Guest Editor
Department of Aerospace and Geodesy, TUM School of Engineering and Design, Technical University of Munich, 85748 Munich, Germany
Interests: unmanned aerial vehicles; system identification; flight dynamics; flight control; bioinspired aerial vehicles; VTOL configurations
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Special Issue Information

Dear Colleagues,

Unmanned aerial vehicles (UAVs) are a rapidly developing technology in the aerospace sector of the 21st century, with applications in aerial photography/mapping, remote monitoring/sensing, surveillance and reconnaissance, infrastructure inspection, etc. Thanks to advances in fields ranging from computation and sensing to new materials and manufacturing methods, UAVs are becoming increasingly more sophisticated, and numerous new UAV applications are being explored, involving operations in challenging environments and requiring high levels of autonomy. The rapid growth in demand for complex UAV missions brings with it a variety of design and performance challenges. Meeting these challenges, in turn, calls for advances in UAV flight dynamics and autonomous control. This Special Issue welcomes papers on ongoing or recently completed research projects in flight dynamics and autonomous control of UAVs. Suggested topics include but are not limited to:

  • UAV flight testing
  • Flight dynamics modeling and simulation of UAVs
  • UAV system identification
  • Advanced control and autonomous capabilities for UAVs
  • Advanced navigation technologies for UAVs
  • Artificial intelligence and machine learning technologies for UAVs
  • Multi-UAV cooperative control

Prof. Dr. Sophie F. Armanini
Guest Editor

Manuscript Submission Information

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Published Papers (1 paper)

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Research

16 pages, 4273 KiB  
Article
Effect of Electric Ducted Fans Structural Arrangement on Their Performance Characteristics
by Daniel Urban, Stanislav Kusmirek, Vladimir Socha, Lenka Hanakova, Karel Hylmar and Jakub Kraus
Appl. Sci. 2023, 13(5), 2787; https://doi.org/10.3390/app13052787 - 21 Feb 2023
Cited by 2 | Viewed by 4573
Abstract
With the expanding electrification in all sectors of transport, it is necessary to look for new efficient solutions for propulsion systems for use in air transport. One of the approaches can be the use of electric ducted fans (EDFs), especially in, but not [...] Read more.
With the expanding electrification in all sectors of transport, it is necessary to look for new efficient solutions for propulsion systems for use in air transport. One of the approaches can be the use of electric ducted fans (EDFs), especially in, but not limited to, the case of unmanned aerial vehicles with vertical takeoff and landing. This concept has been known for several decades but has been used very little and therefore has been almost unexplored. This opens up opportunities for investigating the performance characteristics, electrical consumption or efficient thrust vectoring of EDFs with respect to their design and operational use. The presented study therefore deals with the influence of the EDF design change on its performance characteristics. These design changes mainly concerned the geometry of the cowling, i.e., reduction and increase of outlet cross section, and arrangement of fans, i.e., one- and two-rotor specification. The comparison was based on measuring of vertical thrust and power consumption during static testing. The results showed that the increasing outlet is the most suitable construction for the generation of vertical thrust during static testing, considering the specifically used EDF construction arrangement. Based on the findings, it can also be concluded that EDFs are a suitable option for use in unmanned aircraft as a competition to other propulsion systems. Full article
(This article belongs to the Special Issue Advances in Flight Dynamics and Autonomous Control of UAVs)
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