The invention provides an unmanned aerial vehicle take-off control method, an unmanned aerial vehicle landing control method and related equipment, and relates to the technical field of unmanned aerial vehicles. When the multi-rotor unmanned aerial vehicle receives the take-off instruction and detects that the original fuselage posture of the multi-rotor unmanned aerial vehicle on the unmanned aerial vehicle parking site is in the inclined state, the driving device is controlled to drive the seedling feeding disc to transversely move relative to the fuselage frame of the multi-rotor unmanned aerial vehicle; the offset of the gravity center of the multi-rotor unmanned aerial vehicle relative to the horizontal state in the takeoff process is compensated through transverse movement of the seedling feeding disc, the actual offset of the gravity center of the unmanned aerial vehicle in the takeoff process is reduced, and the takeoff load needing to be overcome by low-side rotors is reduced. And then the multi-rotor unmanned aerial vehicle is controlled to take off from the unmanned aerial vehicle parking site according to the take-off instruction, so that the low-side rotors can provide enough power to ensure stable take-off of the unmanned aerial vehicle, the overturning risk of the unmanned aerial vehicle during take-off in a site with an obvious slope or a site with an uneven ground is effectively reduced, and the take-off stability of the unmanned aerial vehicle is improved.
本申请提供一种无人机起飞控制方法、无人机降落控制方法及相关设备,涉及无人机技术领域。本申请在多旋翼无人机接收到起飞指令,并检测到自身在无人机停放场地上的原始机身姿态处于倾斜状态时,控制驱动装置驱动送秧盘相对于多旋翼无人机的机身框架横向移动,以通过送秧盘横移动作对多旋翼无人机在起飞过程中相对于水平状态的重心偏移量进行补偿,减少无人机重心在起飞过程中的实际偏移量,并降低低侧旋翼需要克服的起飞负荷,然后按照起飞指令控制多旋翼无人机从无人机停放场地起飞,使低侧旋翼能提供足够动力来确保无人机平稳起飞,从而有效降低无人机在具有明显坡度的场地或者地面不平整的场地内起飞时的倾覆风险,提升无人机起飞平稳性。
Unmanned aerial vehicle takeoff control method, unmanned aerial vehicle landing control method and related equipment
无人机起飞控制方法、无人机降落控制方法及相关设备
2025-01-10
Patent
Electronic Resource
Chinese
Rapid takeoff-landing unmanned aerial vehicle and takeoff and landing control method thereof
European Patent Office | 2020
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