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28

example is 60.7 mm in diameter, 39.5

mm in length and weighs 255 g. The

company quotes an idle current of 0.9 A,

a maximum continuous current of 40 A,

maximum continuous power of 1180 W

and an internal resistance of 33 m

Ω

.

The stators are hand-wound at 180 C

from a single thick, oxygen-free copper

wire to enhance resistance to short-

circuits. The housing is machined from

aluminium and the stators are made

from 0.2 mm laminations of silicon steel

for efficiency and minimum eddy current

losses. Stator plates are epoxy coated

to prevent shorts in the windings, and

a stainless steel propeller adapter is

available as an option.

The propeller shaft is designed to

prevent loosening, and the large bearing

has a claimed Mean Time Between

Failures of 160 hours. Integral air cooling

is to a patented design, and the motor

is claimed to be waterproof as well as

resistant to dirt and sand. The motor is

tested to military standards, says T-Motor.

For power and signal distribution from

the batteries to the motors, avionics and

payload, the prototypes are wired up,

but the company is working on a

distribution board/box for production.

This will have a cable connector with

about 20 pins to mate it with the avionics

box, which has other interfaces for

sensors.

PX4-based flight control

De Villiers says the Alti Transition flies much

like a large quadcopter in hover mode

but with less yaw authority; pitch and roll

are very responsive, with yaw taking a little

longer owing to the long wingspan and

lateral mass. The conventional differential

motor speed technique is used for yaw

control in the hover.

To control the aircraft, Alti has

developed its own autopilot based on

the open source PX4 standard with a

companion PC. The PX4 flight stack

is described as a complete control

solution for multicopter and fixed-

wing UAVs, and even ground robots,

while the middleware consists of a

robotics communications toolkit that

the development team calls efficient,

lightweight and “blazing fast”.

Developed from 2009 by the Computer

Vision and Geometry Laboratory at

ETH Zurich, otherwise known as the

Swiss Federal Institute of Technology,

PX4 software is also supported by

the institute’s Autonomous Systems

Laboratory and Automatic Control

Laboratory. It received a further boost

when Qualcomm Technologies adopted

it for its new Snapdragon Flight board,

which forms the core of the Snapdragon

June/July 2016 |

Unmanned Systems Technology

For transport, Transition can be disassembled into four sections – the two outer wings,

fuselage/wing roots and the tail hoop with booms and stabiliser

CAD rendering showing

the engine fairing with

only the cylinder exposed;

detail of rear lift motor that

will be integrated into the

wing centre/fuselage for

production