The Magazine of IEEE-Eta Kappa Nu October 2017 - 26

FEATURE

Fig. 6. Mission Planner user interface

of gravity (CG) with good flight stability characteristics.
Figure 7 shows a diagram of the component placement
regarding the manufacturer's suggested CG point.

Fig. 7. Component placement

The MTD has full control over all three rotation axes
(roll, pitch, and yaw) via ailerons, one on each wing,
and an elevator and rudder, both located on the tail,
for flight control. Propulsion for the MTD is generated by
two brushless motors installed with 30.5-cm propellers
that create a total combined static thrust of 4400 g at
maximum throttle. The total weight of the system is 4.8
kg and has an experimentally verified maximum takeoff
weight of 5.5 kg. The MTD airframe is illustrated as a
three-dimensional SolidWorks model in Figure 8.

Fig. 8. 3D model of MTD in SolidWorks

26

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