VERTICAL TAKE-OFF AND LANDING POSSIBLE FLIGHT BODY, FLIGHT BODY, CONTROLLER AND CONTROL METHOD FOR VERTICAL TAKE-OFF AND LANDING POSSIBLE FLIGHT BODY, AND RECORDING MEDIUM STORING CONTROL PROGRAM

摘要

PROBLEM TO BE SOLVED: To provide a vertical take-off and landing possible flight body of which a possibility of crash can be reduced.;SOLUTION: A vertical take-off and landing possible flight body comprises: an airframe primary part 10; frames 11 to 14 which define a quadrant center in the airframe primary part in a plane pattern, and supports the airframe primary part so as to generate independent lifting power in the same direction to each of a plurality of quadrants around the quadrant center; main propellers 31 to 34 which are located by rotary shafts provided on the frames 11 to 14; and auxiliary propellers 35 to 38 which are located by the rotary shafts provided on the frames in a first quadrant selected among the plurality of quadrants, and have the same rotation direction as those of the main propellers. The rotation direction of the main propeller in another quadrant adjacent to the first quadrant is an opposite direction.;SELECTED DRAWING: Figure 44;COPYRIGHT: (C)2019,JPO&INPIT