Evidence map›Paper›PMID 37268720›Full record

ArticleScientific reports2023

First lift-off and flight performance of a tailless flapping-wing aerial robot in high-altitude environments.

Shu Tsuchiya, Hikaru Aono, Keisuke Asai, Taku Nonomura, Yuta Ozawa, Masayuki Anyoji, Noriyasu Ando, Chang-Kwon Kang, Jeremy Pohly

Open access · goldAbstract read
In one paragraph

Article in Scientific reports, 2023. 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
9.0field-weighted citation impact, top 3% of its field
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, 12 citations in OpenAlex.

  1. Article
  2. Article
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

9 authors at 5 institutions in 2 countries.

Shu TsuchiyaGraduate School of Science and Technology, Shinshu University, Nagano, 3868567, Japan.
Hikaru AonoGraduate School of Science and Technology, Shinshu University, Nagano, 3868567, Japan. aono@shinshu-u.ac.jp.
Keisuke AsaiGraduate School of Engineering, Tohoku University, Miyagi, 9808579, Japan.
Taku NonomuraGraduate School of Engineering, Tohoku University, Miyagi, 9808579, Japan.
Yuta OzawaGraduate School of Engineering, Tohoku University, Miyagi, 9808579, Japan.
Masayuki AnyojiInterdisciplinary Graduate School of Engineering Sciences, Kyushu University, Fukuoka, 8168580, Japan.
Noriyasu AndoDepartment of System Life Engineering, Maebashi Institute of Technology, Gunma, 3710816, Japan.
Chang-Kwon KangDepartment of Mechanical and Aerospace Engineering, University of Alabama in Huntsville, Huntsville, AL, 35899, USA.
Jeremy PohlyDepartment of Mechanical and Aerospace Engineering, University of Alabama in Huntsville, Huntsville, AL, 35899, USA.
Tohoku University · JPShinshu University · JPUniversity of Alabama in Huntsville · USKyushu University · JPMaebashi Institute of Technology · JP

Funding

MEXT | Japan Society for the Promotion of Science (JSPS) JP19H00800MEXT | Japan Society for the Promotion of Science (JSPS) JP22H01397National Aeronautics and Space Administration (NASA) 80NSSC18K0870NSF | ENG/OAD | Division of Civil, Mechanical and Manufacturing Innovation (CMMI) CMMI-1761618
6 · The paper itself

Abstract

Flapping flight of animals has captured the interest of researchers due to their impressive flight capabilities across diverse environments including mountains, oceans, forests, and urban areas. Despite the significant progress made in understanding flapping flight, high-altitude flight as showcased by many migrating animals remains underexplored. At high-altitudes, air density is low, and it is challenging to produce lift. Here we demonstrate a first lift-off of a flapping wing robot in a low-density environment through wing size and motion scaling. Force measurements showed that the lift remained high at 0.14 N despite a 66% reduction of air density from the sea-level condition. The flapping amplitude increased from 148 to 233 degrees, while the pitch amplitude remained nearly constant at 38.2 degrees. The combined effect is that the flapping-wing robot benefited from the angle of attack that is characteristic of flying animals. Our results suggest that it is not a simple increase in the flapping frequency, but a coordinated increase in the wing size and reduction in flapping frequency enables the flight in lower density condition. The key mechanism is to preserve the passive rotations due to wing deformation, confirmed by a bioinspired scaling relationship. Our results highlight the feasibility of flight under a low-density, high-altitude environment due to leveraging unsteady aerodynamic mechanisms unique to flapping wings. We anticipate our experimental demonstration to be a starting point for more sophisticated flapping wing models and robots for autonomous multi-altitude sensing. Furthermore, it is a preliminary step towards flapping wing flight in the ultra-low density Martian atmosphere.

Identifiers

PMID37268720
PMCPMC10238405
OpenAlexW4379197244

What OpenQuestion holds

Textmetadata
LicenceCC BY
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.