Results 151 to 160 of about 8,095 (215)

CGull: A Non-Flapping Bioinspired Composite Morphing Drone. [PDF]

Biomimetics (Basel)
Bishay PL, Rini A, Brambila M, Niednagel P, Eghdamzamiri J, Yousefi H, Herrera J, Saad Y, Bertuch E, Black C, Hanna D, Rodriguez I.   +11 more
europepmc   +1 more source

Research on Deployable Wings for MAVs Bioinspired by the Hind Wings of the Beetle Protaetia brevitarsis. [PDF]

Biomimetics (Basel)
Sun J, Wang W, Li P, Zhang Z.
europepmc   +1 more source

Distributed State Estimation for Flapping-Wing Micro Air Vehicles with Information Fusion Correction. [PDF]

Biomimetics (Basel)
Zhang X, Luo M, Guo S, Cui Z.
europepmc   +1 more source

Aerodynamic and Inertial Loading Effects of Insect-Inspired Appendages in Small Unmanned Aerial Vehicles. [PDF]

Biomimetics (Basel)
Ogunwa T, Chahl J.
europepmc   +1 more source

Effect of the shape of flapping airfoils on aerodynamic forces. [PDF]

Heliyon
Butt F, Talha T, Khan R, Mazhar AR, Butt M, Petru J, Seikh AH.   +6 more
europepmc   +1 more source

The evaluation of animal welfare indicators based on transport duration and lighting differences in the slaughter of broiler chickens. [PDF]

Open Vet J
Siska W, Latif H, Purnawarman T.
europepmc   +1 more source

Recent Advances in Dielectric Elastomer Actuator-Based Soft Robots: Classification, Applications, and Future Perspectives. [PDF]

Gels
Li S, Gao Z, Yang W, Wang R, Zhang L.
europepmc   +1 more source

Attention-Based Multi-Objective Control for Morphing Aircraft. [PDF]

Biomimetics (Basel)
Fu Q, Sun C.
europepmc   +1 more source

Biomimetic Wings for Micro Air Vehicles. [PDF]

Biomimetics (Basel)
Moscato G, Romano GP.
europepmc   +1 more source

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Camber-adjustable flapping wing air vehicles

2011 8th International Conference on Ubiquitous Robots and Ambient Intelligence (URAI), 2011
This paper introduces the implementation of adjustable camber of flapping wing and tail of a typical artificial flapping vehicle using a flexible piezoelectric actuator, called macro-fiber composites (MFC). When MFC is applied to the main wing of an ornithopter, the induced camber greatly affects aerodynamic characteristics such as mean lift and thrust.
null Jun-Seong Lee, null Jae-Hung Han, null Dae-Kwan Kim   +2 more
openaire   +1 more source