Evidence map›Paper›PMID 40442170›Full record

ArticleScientific reports2025

Multi-criteria decision model for multicircular flight control of unmanned aerial vehicles through a hybrid approach.

Noorulden Basil, Hamzah M Marhoon, Bayan Mahdi Sabbar, Abdullah Fadhil Mohammed, Osamah Albahri, Ahmed Albahri, Abdullah Alamoodi, Iman Mohamad Sharaf, Amare Merfo Amsal, Mahrous Ahmed and 2 more

Abstract read
In one paragraph

Article in Scientific reports, 2025. The graph could read no effect estimate from its abstract, so it casts no vote on the map. Cited by 2 papers.

0numbers the graph read from it
0cells of the map it votes in
2citing 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

2 citing papers in PubMed.

  1. Article
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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

12 authors.

Noorulden BasilDepartment of Electrical Engineering, College of Engineering, Mustansiriyah University, Baghdad, Iraq. noorulden@uomustansiriyah.edu.iq.
Hamzah M MarhoonDepartment of Automation Engineering and Artificial Intelligence, College of Information Engineering, Al-Nahrain University, Jadriya, Baghdad, Iraq.
Bayan Mahdi SabbarCollege of Engineering and Engineering Techniques, Al-Mustaqbal University, Babylon, Iraq.
Abdullah Fadhil MohammedDepartment of Electrical Engineering, College of Engineering, Mustansiriyah University, Baghdad, Iraq.
Osamah AlbahriComputer Techniques Engineering Department, Mazaya University College, Nasiriyah, Iraq.
Ahmed AlbahriTechnical Engineering College, Imam Ja'afar Al-Sadiq University (IJSU), Baghdad, Iraq.
Abdullah AlamoodiApplied Science Research Center, Applied Science Private University, Amman, Jordan.
Iman Mohamad SharafDepartment of Basic Sciences, Higher Technological Institute, 10th of Ramadan City, Egypt.
Amare Merfo AmsalDepartment of Mechanical Engineering, Faculty of Technology, Debre Markos University, P. O. Box 269, Debre Markos, Ethiopia. amare_merfo@dmu.edu.et.
Mahrous AhmedDepartment of Electrical Engineering, College of Engineering, Taif University, 21944, Taif, Saudi Arabia.
Enas AliCentre for Research Impact and Outcome, Chitkara University Institute of Engineering and Technology, Chitkara University, Rajpura, Punjab, 140401, India.
Sherif S M GhoneimDepartment of Electrical Engineering, College of Engineering, Taif University, 21944, Taif, Saudi Arabia.

Funding

No grant is acknowledged in the PubMed record.

6 · The paper itself

Abstract

This study presents a novel approach for optimizing UAV (unmanned aerial vehicle) Multicircular flight control by developing a fractional order proportional integral derivative (FOPID)-based hybrid Eagle strategy particle swarm optimization ant lion optimizer (HESPSOALO). The proposed algorithm combines the strengths of particle swarm optimization (PSO) and the ant lion optimizer (ALO), which are enhanced by the Eagle strategy to systematically fine-tune the FOPID controller parameters. This hybrid optimization method aims to improve system stability, responsiveness, and disturbance rejection in UAVs, particularly in challenging dynamic flight conditions. The proposed approach was validated against traditional control methods that utilize FOPID (Base), the Base HESPSOALO algorithm, the FOPID-based HPSOGWO (Hybrid Particle Swarm Optimization-Gray Wolf Optimizer), and the FOPID-based HGWOALO (Hybrid Gray Wolf Optimization-Ant Lion Optimizer) with a set of benchmark functions used in the analysis. The results demonstrate a minimization of position and angular errors, reduced oscillations, and overall improved control stability for the FOPID-based HESPSOALO compared with the other methods. Furthermore, a multicriteria decision-making (MCDM) framework is applied to evaluate the overall performance of alternative control strategies utilizing the CRiteria importance through intercriteria correlation (CRITIC) and technique of order preference by similarity to ideal solution (TOPSIS) techniques. The MCDM analysis demonstrates that among the evaluated criteria, [Formula: see text] has the highest importance, with a weight of 0.244019, whereas [Formula: see text] is deemed the least significant, with a weight of 0.161023. The ranking results reveal that the HESPSOALO algorithm (Base) is the best-performing controller method, with a ranking score of 0.571161, indicating its superior control performance across major metrics. In contrast, the FOPID + HPSOGWO controller method ranks the lowest, with a score of 0.282794. The findings have significant industrial implications, particularly in sectors where UAVs are critical for precision tasks, such as logistics, agriculture, surveillance, and environmental monitoring. By optimizing the FOPID controller parameters, the HESPSOALO algorithm enhances UAV stability, responsiveness, and reliability in dynamic environments, resulting in more precise control and robust performance under varying conditions. This improvement may reduce operational risks and maintenance costs while increasing efficiency, prolonging UAV service life, and achieving energy savings. This study provides a robust solution for UAV control based on the potential of hybrid optimization algorithms to improve UAV precision and reliability in autonomous flight.

Indexed as

CRITICFOPIDHybrid optimizationTOPSISUAV multicircular flight control

Identifiers

PMID40442170
PMCPMC12122686

What OpenQuestion holds

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LicenceCC BY-NC-ND
Read underepoch 390

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.