Evidence map›Paper›PMID 41549117›Full record

ArticleScientific reports2026

Fuzzy logic based nonlinear blending hybrid control of a kestrel-inspired ornithopter operating in sinusoidal and dryden gusts.

S H Abbasi, Abdul Khader Jilani Saudagar, A Nouman, Mamoun Lyes Hennache

Abstract read
In one paragraph

Article in Scientific reports, 2026. The graph could read no effect estimate from its abstract, so it casts no vote on the map. Not yet cited in PubMed.

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

0 citing papers in PubMed.

No citing paper in PubMed yet.

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

4 authors.

S H AbbasiDepartment of Electrical and Computer Engineering, SS CASE IT, Islamabad, Pakistan. abbasi882@gmail.com.ORCID http://orcid.org/0000-0002-3443-8284
Abdul Khader Jilani SaudagarInformation Systems Department, College of Computer and Information Sciences, Imam Mohammad Ibn Saud Islamic University (IMSIU), Riyadh, 11432, Saudi Arabia.ORCID http://orcid.org/0000-0003-4205-3621
A NoumanDepartment of Mechanical Engineering, National University of Sciences and Technology, Islamabad, Pakistan.ORCID http://orcid.org/0009-0008-1829-8702
Mamoun Lyes HennacheElectrical Engineering Department, King Fahd University of Petroleum and Minerals, Dhahran, Saudi Arabia.ORCID http://orcid.org/0000-0001-8007-9094

Funding

Deanship of Scientific Research, Imam Mohammed Ibn Saud Islamic University IMSIU-DDRSP2503
6 · The paper itself

Abstract

Persistent gust disturbances and unsteady atmospheric dynamics remain a critical barrier to the stable and efficient flight of ornithopters. However, in nature, millions of avian species exhibit extraordinary inherent stability and aerodynamic adaptability, even under highly turbulent atmospheric conditions. Experimental studies have shown that birds actively deploy their covert feathers to dynamically modulate airflow and suppress gust-induced disturbances. Inspired by this biological mechanism, this study proposes a biomimetic Gust Alleviation System (GAS) integrated with a hybrid control framework for a kestrel-inspired ornithopter. The GAS is modeled using a reduced-order bond graph representation and actively modulates feather-like surfaces for aerodynamic load mitigation. An optimal Linear Quadratic Regulator (LQR) governs nominal gusts, while a robust [Formula: see text] controller is engaged for stronger gusts. A nonlinear fuzzy Sugeno-type blending mechanism is introduced to ensure smooth and shock-free transition between controllers in the intermediate gust regime. In addition to step-gust testing, the proposed system is evaluated under sinusoidal disturbances and realistic Dryden wind turbulence models, where it consistently maintains bounded, well-damped, and stable responses. The results demonstrate up to 50% reduction in gust-induced forces, 36% improvement in control efficiency, and 24% enhancement in robustness compared to conventional methods, while remaining fully aligned with literature-reported ornithopter dynamics. This biologically inspired GAS with fuzzy-blended hybrid control offers a reliable, energy-efficient, and aerodynamically resilient solution for next-generation ornithopters operating in unsteady atmospheric environments.

Identifiers

PMID41549117
PMCPMC12815933

What OpenQuestion holds

Textmetadata
LicenceCC BY-NC-ND
Read underepoch 390

Registered trials

None linked

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.