Mar
07
2018
The speed of the sUAS is determined by the aircraft and sensor limitations. Multirotor aircraft are more adaptable to speeds which typically range from 5-9m/s. At a minimum, they can hover in place and increase in speed up to the limitation of the specific system. Fixed-wing aircraft are less adaptable, as they always require forward movement and maximum and minimum speeds are dependent on each specific system. Sensor limitations are related to the desired overlap as stated in the previous tab.
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