Insect-scale Flapping-wing Micro Research Articles

Analysing the Aerodynamic Performance of Dragonfly-Inspired Wing in Forward Flight: A Computational Approach

This paper presents a numerical investigation into the forward flight dynamics of a dragonfly-inspired wing. A three-dimensional (3-D) profiled wing model, specifically the right hind wing, was utilized for simulations. The wing model featured a tapering thickness from the wing root to the wing tip and from the leading edge to the trailing edge, replicating the morphological characteristics observed in dragonfly wings. Morphological data were acquired using a digital micrometre instrument, DSLR camera and Scanning Electron Microscope. The study aimed to evaluate the impact of advance ratio on the aerodynamic performance of the dragonfly-inspired wing during forward flight. Analysis was conducted on a single-degree-of-freedom flapping mechanism, with a flapping frequency set at 36 Hz to mimic the natural wingbeat frequency of a dragonfly. Results revealed a notable pressure disparity between the upper and lower surfaces during the downstroke, indicative of substantial lift generation during flapping motion. Additionally, the visualization of the leading-edge vortex formation provided further insights into the aerodynamic mechanisms at play. Overall, this study contributes valuable insights into the aerodynamic performance of insect-scale flapping wing micro air vehicles, offering potential advancements in their design and development

A Review of Propulsion, Power, and Control Architectures for Insect-Scale Flapping-Wing Vehicles

Flying insects are able to navigate complex and highly dynamic environments, can rapidly change their flight speeds and directions, are robust to environmental disturbances, and are capable of long migratory flights. However, flying robots at similar scales have not yet demonstrated these characteristics autonomously. Recent advances in mesoscale manufacturing, novel actuation, control, and custom integrated circuit (IC) design have enabled the design of insect-scale flapping wing micro air vehicles (MAVs). However, there remain numerous constraints to component technologies—for example, scalable high-energy density power storage—that limit their functionality. This paper highlights the recent developments in the design of small-scale flapping wing MAVs, specifically discussing the various power and actuation technologies selected at various vehicle scales as well as the control architecture and avionics onboard the vehicle. We also outline the challenges associated with creating an integrated insect-scale flapping wing MAV.

Artificial insect wings with biomimetic wing morphology and mechanical properties

The pursuit of a high lift force for insect-scale flapping-wing micro aerial vehicles (FMAVs) requires that their artificial wings possess biomimetic wing features which are close to those of their natural counterpart. In this work, we present both fabrication and testing methods for artificial insect wings with biomimetic wing morphology and mechanical properties. The artificial cicada (Hyalessa maculaticollis) wing is fabricated through a high precision laser cutting technique and a bonding process of multilayer materials. Through controlling the shape of the wing venation, the fabrication method can achieve three-dimensional wing architecture, including cambers or corrugations. Besides the artificial cicada wing, the proposed fabrication method also shows a promising versatility for diverse wing types. Considering the artificial cicada wing’s characteristics of small size and light weight, special mechanical testing systems are designed to investigate its mechanical properties. Flexural stiffness, maximum deformation rate and natural frequency are measured and compared with those of its natural counterpart. Test results reveal that the mechanical properties of the artificial cicada wing depend strongly on its vein thickness, which can be used to optimize an artificial cicada wing’s mechanical properties in the future. As such, this work provides a new form of artificial insect wings which can be used in the field of insect-scale FMAVs.

Low-voltage electromagnetic actuators for flapping-wing micro aerial vehicles

This paper presents a new type of electromagnetic actuator driven by a low voltage of 5.5V for potential applications in insect scale Flapping-wing Micro Aerial Vehicles (FMAVs). The actuator can generate vibratory motions via cantilever-beam or cantilever-plate structures to drive artificial wings through flapping motion. The induced magnetic Lorentz force is analyzed by a simplified lumped mass model and the dynamic characteristics including resonant frequency and amplitude are investigated through experimental tests. In the prototype designs and tests, a peak amplitude of 29.8mm from a 25mm-long cantilever beam structure has been achieved. Furthermore, a prototype device with the cantilever beam actuator using small magnets of 197.2mg has demonstrated 5.7 times higher output power density at 0.56W/Kg as compared with that of another prototype device using larger magnets of 2409.2mg. This implies the potential for further miniaturized systems toward FMAVs. Under a driving voltage of 5.5V, a cantilever plate actuator has been shown to drive a pair of artificial wings to achieve 20° flapping amplitude at 101.4Hz, which results in a high power density of 9.52W/Kg. By applying AC current to a planar coil, the power density of the actuator can be further enhanced to 48.56W/Kg. As such, the low-voltage electromagnetic actuators could broaden the driving mechanisms for insect scale FMAVs.

An Improved Evolvable Oscillator and Basis Function Set for Control of an Insect-Scale Flapping-Wing Micro Air Vehicle

This paper introduces an improved evolvable and adaptive hardware oscillator design capable of supporting adaptation intended to restore control precision in damaged or imperfectly manufactured insect-scale flapping-wing micro air vehicles. It will also present preliminary experimental results demonstrating that previously used basis function sets may have been too large and that significantly improved learning times may be achieved by judiciously culling the oscillator search space. The paper will conclude with a discussion of the application of this adaptive, evolvable oscillator to full vehicle control as well as the consideration of longer term goals and requirements.

A comparative study of dragonfly inspired flapping wings actuated by single crystal piezoceramic

A dragonfly inspired flapping wing is investigated in this paper. The flapping wing is actuated from the root by a PZT-5H and PZN-7%PT single crystal unimorph in the piezofan configuration. The nonlinear governing equations of motion of the smart flapping wing are obtained using the Hamilton's principle. These equations are then discretized using the Galerkin method and solved using the method of multiple scales. Dynamic characteristics of smart flapping wings having the same size as the actual wings of three different dragonfly species Aeshna Multicolor, Anax Parthenope Julius and Sympetrum Frequens are analyzed using numerical simulations. An unsteady aerodynamic model is used to obtain the aerodynamic forces. Finally, a comparative study of performances of three piezoelectrically actuated flapping wings is performed. The numerical results in this paper show that use of PZN-7%PT single crystal piezoceramic can lead to considerable amount of wing weight reduction and increase of lift and thrust force compared to PZT-5H material. It is also shown that dragonfly inspired smart flapping wings actuated by single crystal piezoceramic are a viable contender for insect scale flapping wing micro air vehicles.

Ionic Polymer Metal Composite Flapping Actuator Mimicking Dragonflies

In this study, variational principle is used for dynamic modeling of an Ionic Polymer Metal Composite (IPMC) flapping wing. The IPMC is an Electro-active Polymer (EAP) which is emerging as a useful smart material for `artificial muscle' applications. Dynamic characteristics of IPMC flapping wings having the same size as the actual wings of three different dragonfly species Aeshna Multicolor, Anax Parthenope Julius and Sympetrum Frequens are analyzed using numerical simulations. An unsteady aerodynamic model is used to obtain the aerodynamic forces. A comparative study of the performances of three IPMC flapping wings is conducted. Among the three species, it is found that thrust force produced by the IPMC flapping wing of the same size as Anax Parthenope Julius wing is maximum. Lift force produced by the IPMC wing of the same size as Sympetrum Frequens wing is maximum and the wing is suitable for low speed flight. The numerical results in this paper show that dragonfly inspired IPMC flapping wings are a viable contender for insect scale flapping wing micro air vehicles.