Table of Contents Table of Contents
Previous Page  90 / 92 Next Page
Information
Show Menu
Previous Page 90 / 92 Next Page
Page Background

90

June/July 2016 |

Unmanned Systems Technology

PS

|

The Robotic Hummingbird

G

iven the current requirement

for bird-sized unmanned air

vehicles for surveillance and

similar applications, coupled

with our understanding of

aerodynamics and the latest advancements

in microelectronics and power sources,

designers are now able to miniaturise

flying craft down to a size that is feasible for

flapping wing flight (writes Stewart Mitchell).

David Colman, of the Department

of Aerospace Engineering at Texas

A&M University, has been researching

this area, and he says “Our recent

investigations have proved that biological

flapping wing flight offers superior

manoeuvrability with excellent gust

tolerance and disturbance rejection

capabilities compared with that of

conventional craft.

“Also, flapping wings use several

unsteady aerodynamic phenomena, such

as leading-edge vortices, at low Reynolds

numbers [air boundary layer flow

separation caused by turbulence], that

significantly enhance lift production over

what is seen in steady flow conditions

such as those on conventional aircraft.”

After research into the potential of a

flapping wing micro air vehicle (MAV) in

early 2015, Colman and his colleagues

at the university designed, manufactured

and tested a biologically inspired two-

winged, hover-capable autonomous MAV

which they call the Robotic Hummingbird.

It has a wingspan of 12 in and flaps

at 22 Hz to manoeuvre its 62 g weight.

Wing control is taken care of by a unique

modified five-bar crank-rocker system,

which turns the rotary motion of the

motor into a linear arc (flapping) motion.

The system is similar in principle to a

four-bar crank-rocker linkage but with

an extra shaft that enhances the flapping

amplitude and modulates the right- and

left-wing flapping speed and amplitude

independently. It also means the MAV

can provide more lift than any other

flapping wing aircraft of its size, and has

much more intricate aerial control.

Each wing is made from a lightweight

plastic material, and weighs only 0.85 g.

The wings also have flexible spars that

aid lift by using aeroelasticity, flexing so

as to increase their lift area. A modular

mechanism controls each wing’s flapping

frequency and amplitude independently to

keep it true to its orientation and direction

along a specified course or to hover.

The MAV’s control system incorporates

an autopilot, which auto-stabilises the

craft from almost any orientation using the

response from a series of high feedback-

rate gyros and sensors on board.

“The biggest challenge was to develop

a design with the strength throughout its

components to withstand the large forces

imposed during flapping,” says Colman.

To that end, the main body of the

vehicle, which functions as an anchor

point for all the mechanical subsystems

– including a 29 KV brushless dc motor,

flapping mechanism, actuators and wing

kinematic modulation device – is rapid

prototyped from ABS plastic, giving it a

weight of only 5.3 g. A 2.75 mm diameter

carbon fibre rod protrudes vertically

down from the body to support the base

of the craft on landing.

Results from flight tests on the

Hummingbird in a small enclosure show

that it has better hovering and turning

capabilities than other contemporary

MAVs, which could mean that in the

future we may see MAVs with the same

agility as nature’s own hummingbird.

Now,

here’s a

thing

The biggest

challenge was

to develop a

design with

the strength to

withstand the

large forces

during flapping