CPC G08G 5/006 (2013.01) [G05D 1/0202 (2013.01); G08G 5/0021 (2013.01); G08G 5/0052 (2013.01); G08G 5/0069 (2013.01)] | 20 Claims |
1. An unmanned aerial vehicle (“UAV”), the UAV comprising:
an electric speed controller interfaced with thrust motors of the UAV; and
a flight controller configured to:
determine a geographic location and a velocity of the UAV, wherein the velocity includes a first component and a second component;
determine a distance between the geographic location of the UAV and a closest segment of a no-fly zone;
determine a zone of deceleration, the zone of deceleration comprising a distal section and a proximal section; and
in response to the UAV crossing a switch point located at an intersection of the distal section and the proximal section, changing a deceleration rate of the UAV from a first deceleration rate to a second deceleration rate by the electric speed controller adjusting the thrust motors.
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