Unmanned aerial vehicle and landing system

An unmanned aerial vehicle, comprising:

• a vehicle body, the vehicle body comprising a front end, a rear end opposite the front end, and a longitudinal axis between the front end and the rear end, the vehicle body further comprising an airfoil shape and at least one wing formed by the vehicle body;
• a plurality of rotors disposed at the front end of the vehicle body, each rotor comprises at least one attached propeller blade, the plurality of rotors being operative to provide forward thrust in a direction of the longitudinal axis;
• a payload void, the payload void being formed by the vehicle body and disposed within the airfoil shape of the vehicle body, the payload void comprising a majority of a volume of the vehicle body;
• a payload bay, the payload bay configured to receive a payload, the payload bay being disposed at least partially within the payload void;
• and
• a flight control system, the flight control system comprising:
• at least one motor to drive the plurality of rotors;
• at least one accelerometer;
• at least one gyro;
• and
• a control module configured to lift and lower the vehicle in a tail-sitter orientation, transition between a tail-sitter orientation and a winged flight orientation, and control a winged flight.