| 摘要 |
<p>PROBLEM TO BE SOLVED: To enable attitude control to be performed easily and quickly in a flight vehicle (multicopter) with plural multiblade rotors (propellers).SOLUTION: A vertical take-off and landing flight vehicle comprises: a plurality of inner rotor units (RU11-RU14) arranged on a first circumference separated from the center of an airframe by a predetermined distance; a plurality of outer rotor units (RU21-RU24) arranged on a second circumference separated from the center of the airframe by a predetermined distance larger than the predetermined distance; and control means for drivingly controlling the inner rotor units and the outer rotor units. Flotation of the air frame is performed by operating mainly the inner rotor units (RU11-RU14) and attitude control of the airframe is performed by operating mainly the outer rotor units (RU21-RU24).</p> |
