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A drone tough lift-off and landing vertical optimized for missions in complex environment

机译:针对复杂环境中的任务优化的无人驾驶飞机艰难的起降垂直

摘要

The present invention relates to a self-contained device forming an aircraft on take-off and landing, capable of advancing flight and of stationary flight, comprising: - a fuselage (2), two flanges (3, 4), the monitoring means of an environment, a propulsion unit (7) mounted at the rear end of the fuselage, a lifting unit (6) mounted at the front of the fuselage, the propulsion unit and / or the lifting unit being movable / s, by pivoting about the transverse axis, two balancing units (8, 9) which are each mounted at one end of a wing and movable in pivoting about the transverse axis and means for estimating the direction and wind speed, altitude and attitude of the device - a control box, using a control law as a function of the measurements taken by the sensors for: ∘ modify the power and / or the tilt about the transverse axis of at least one balancing unit side and ‘ modify the power and / or the tilt about the transverse axis of at least the propulsion unit and / or support.
机译:本发明涉及一种能够在飞机的起飞和降落时形成飞机的自给式装置,该装置能够推进飞行和静止飞行,包括:-机身(2),两个凸缘(3、4),监测装置。环境,安装在机身后端的推进单元(7),安装在机身前部的提升单元(6),推进单元和/或提升单元可通过围绕横轴,两个平衡单元(8、9),它们分别安装在机翼的一端,并可以绕横轴枢转,并且还具有估算装置的方向和风速,高度和姿态的装置-控制箱,根据传感器的测量结果使用控制定律进行以下操作:∘修改至少一个平衡单元侧面的功率和/或围绕横轴的倾斜度,并'修改功率和/或围绕横轴的倾斜度至少是推进装置和/或支撑装置。

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