To provide an unmanned aerial vehicle capable of stably flying even in the time of approaching a target element.SOLUTION: An unmanned aerial vehicle according to the present disclosure comprises: multiple rotary wings; a body part which has at least a control device that controls the multiple rotary wings; and multiple inclination mechanisms which are equipped with the multiple rotary wings and tilt the multiple rotary wings relative to the body part. The multiple inclination mechanisms include a first inclination mechanism and a second inclination mechanism which are positioned on opposite sides with the body part held therebetween. The multiple rotary wings include a first rotary wing and a second rotary wing respectively mounted on the first inclination mechanism and the second inclination mechanism. The control device utilizes a distance measurement sensor to measure the distance to target elements around the unmanned aerial vehicle, controls the first inclination mechanism so that a discharge direction of the air of the first rotary wing is oriented to the target element according to the distance to the target element, and controls the second inclination mechanism so that the discharge direction of the air of the second rotary wing is oriented to the opposite direction to the target element.SELECTED DRAWING: Figure 1
【課題】対象要素への接近状態時においても、安定した飛行を行うことができる無人飛行体を提供する。【解決手段】本開示に係る無人飛行体は、複数の回転翼と、複数の回転翼を制御する制御装置を少なくとも有した本体部と、複数の回転翼を搭載し、複数の回転翼を前記本体部に対して傾斜させる複数の傾斜機構と、を備え、複数の傾斜機構は、本体部を間に挟んで互いに反対側に位置する第1の傾斜機構および第2の傾斜機構を有し、複数の回転翼は、第1の傾斜機構および第2の傾斜機構にそれぞれ搭載される第1の回転翼および第2の回転翼を有し、制御装置は、距離測定センサによって無人飛行の周辺の対象要素までの距離を測定し、対象要素との距離に応じて、第1の回転翼の空気の排出方向が対象要素に向くように、第1の傾斜機構を制御すると共に、第2の回転翼の空気の排出方向が対象要素とは反対方向に向くように、第2の傾斜機構を制御する。【選択図】図1
UNMANNED AERIAL VEHICLE AND FLIGHT CONTROL METHOD FOR UNMANNED AERIAL VEHICLE
無人飛行体および無人飛行体の飛行制御方法
26.12.2024
Patent
Elektronische Ressource
Japanisch
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