Evidence map›Paper›PMID 35897981›Full record

ArticleSensors (Basel, Switzerland)2022

Quality-of-Service-Centric Design and Analysis of Unmanned Aerial Vehicles.

Sudhanshu Kumar Jha, Shiv Prakash, Rajkumar Singh Rathore, Mufti Mahmud, Omprakash Kaiwartya, Jaime Lloret

Abstract read
In one paragraph

Article in Sensors (Basel, Switzerland), 2022. The graph could read no effect estimate from its abstract, so it casts no vote on the map. Cited by 7 papers.

0numbers the graph read from it
0cells of the map it votes in
7citing papers in PubMed
–field-weighted citation impact
1 · What the graph read from it

What it found

Each row is one number read from the abstract, on the scale the paper reported it, with its interval. Left of the dashed line favours the treatment, right favours the comparator. Under each row is the sentence it came from. New to these charts? A ten-minute tutorial.

The abstract states no effect estimate the extractor could read, or names no intervention and outcome on the map, so this paper lights no cell and moves no belief. It is still indexed, cited and linked below.

2 · The registry

The trial behind it

Trials whose registry record cites this paper, or whose number appears in the abstract. A trial that started after this paper was published is citing it as background, not reporting it.

Neither the registry nor the abstract names a trial number. If this is a trial report, that itself is worth knowing.

3 · Its place in the literature

Who cites it

7 citing papers in PubMed.

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4 · The record

Corrections and comments

PubMed lists nothing against this paper. Absence here is not a guarantee, only a check that was made.

5 · Who and what money

Authors and funding

6 authors.

Sudhanshu Kumar JhaDepartment of Electronics and Communication, University of Allahabad, Prayagraj 211002, Uttar Pradesh, India.
Shiv PrakashDepartment of Electronics and Communication, University of Allahabad, Prayagraj 211002, Uttar Pradesh, India.
Rajkumar Singh RathoreDepartment of Computer Science, Cardiff School of Technologies, Cardiff Metropolitan University, Cardiff Llandaff Campus, Cardiff CF5 2YB, UK.ORCID 0000-0003-4571-1888
Mufti MahmudDepartment of Computer Science, Nottingham Trent University, Clifton Campus, Nottingham NG11 8NS, UK.ORCID 0000-0002-2037-8348
Omprakash KaiwartyaDepartment of Computer Science, Nottingham Trent University, Clifton Campus, Nottingham NG11 8NS, UK.ORCID 0000-0001-9669-8244
Jaime LloretDepartment of Communications, Universitat Politècnica de València, 46022 Valencia, Spain.ORCID 0000-0002-0862-0533

Funding

Notthingham Trent University 00
6 · The paper itself

Abstract

Recent years have witnessed rapid development and great indignation burgeoning in the unmanned aerial vehicles (UAV) field. This growth of UAV-related research contributes to several challenges, including inter-communication from vehicle to vehicle, transportation coverage, network information gathering, network interworking effectiveness, etc. Due to ease of usage, UAVs have found novel applications in various areas such as agriculture, defence, security, medicine, and observation for traffic-monitoring applications. This paper presents an innovative drone system by designing and developing a blended-wing-body (BWB)-based configuration for next-generation drone use cases. The proposed method has several benefits, including a very low interference drag, evenly distributed load inside the body, and less radar signature compared to the state-of-the-art configurations. During the entire procedure, a standard design approach was followed to optimise the BWB framework for next-generation use cases by considering the typically associated parameters such as vertical take-off and landing and drag and stability of the BWB. Extensive simulation experiments were performed to carry out a performance analysis of the proposed model in a software-based environment. To further confirm that the model design of the BWB-UAV is fit to execute the targeted missions, the real-time working environments were tested through advanced numerical simulation and focused on avoiding cost and unwanted wastages. To enhance the trustworthiness of this said computational fluid dynamics (CFD) analysis, grid convergence test-based validation was also conducted. Two different grid convergence tests were conducted on the induced velocity of the Version I UAV and equivalent stress of the Version II UAV. Finite element analysis-based computations were involved in estimating structural outcomes. Finally, the mesh quality was obtained as 0.984 out of 1. The proposed model is very cost-effective for performing a different kind of manoeuvring activities with the help of its unique design at reasonable mobility speed and hence can be modelled for high-speed-based complex next-generation use cases.

Indexed as

AircraftUnmanned Aerial DevicesAgricultureData Collectionblended wing bodyquality of serviceUAV designunmanned aerial vehicles

Identifiers

PMID35897981
PMCPMC9331645

What OpenQuestion holds

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LicenceCC BY
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Registered trials

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Read under generation 80e0d062 · epoch 390. Bibliography from PubMed, PubMed Central and OpenAlex; grants from NIH RePORTER; trial links from ClinicalTrials.gov; estimates, votes and beliefs from the OpenQuestion graph.