2015
DOI: 10.1260/1756-8293.7.1.21
|View full text |Cite
|
Sign up to set email alerts
|

Free Flight Testing and Performance Evaluation of a Passively Morphing Ornithopter

Abstract: Unmanned Aerial Vehicles (UAVs) are proliferating in both the civil and military markets. Flapping wing UAVs, or ornithopters, have the potential to combine the agility and maneuverability of rotary wing aircraft with excellent performance in the low Reynolds number flight regimes. The purpose of this paper is to present new free flight experimental results for an ornithopter equipped with single degree of freedom compliant spines. The compliant spines are designed and optimized in terms of mass, maximum von-M… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1

Citation Types

1
13
0

Year Published

2017
2017
2022
2022

Publication Types

Select...
6

Relationship

1
5

Authors

Journals

citations
Cited by 14 publications
(14 citation statements)
references
References 24 publications
1
13
0
Order By: Relevance
“…This not only revises our textbook understanding of avian functional morphology [5,6,19], but may critically inform fossil interpretation [29] and developmental studies [22,23]. Finally, the six-bar model offers the first quantitative information for avian-inspired morphing wing design [30][31][32][33].…”
Section: Introductionmentioning
confidence: 68%
See 1 more Smart Citation
“…This not only revises our textbook understanding of avian functional morphology [5,6,19], but may critically inform fossil interpretation [29] and developmental studies [22,23]. Finally, the six-bar model offers the first quantitative information for avian-inspired morphing wing design [30][31][32][33].…”
Section: Introductionmentioning
confidence: 68%
“…crossed four-bar model offer quantitative inspiration for engineering morphing wing design [30][31][32][33].…”
mentioning
confidence: 99%
“…Bats perform less well than high-performance birds, in several metrics, but they are mostly on par with pigeons [159]. Data for scoring from [14,141,[159][160][161][162][163].…”
Section: Robotic Kinematics and Performancementioning
confidence: 99%
“…The solid spar configuration served as a baseline for the ornithopter structure, as well as to determine suitable values for the spar properties such as modulus of elasticity and structural damping coefficient. The CCM designs were based on a compliant spine featuring two compliant joints, which has been tested previously (COMP04PM) [10,32,33]. CSA has the same design parameters and dimensions as the previously tested compliant spine, and CSB has the same design parameters but has been shortened to reduce the mass, and thereby reducing the rotational inertia penalty.…”
Section: Configurations Fabricated For Experiments Andmentioning
confidence: 99%
“…CSB was placed at 40% of the distance. The 40% location is based on the insertion location during the previous benchtop and free flight experiments using COMP04PM [10,33], and was chosen previously based on the location of a typical bird elbow joint (40% of the half wingspan).…”
Section: Configurations Fabricated For Experiments Andmentioning
confidence: 99%