The embodiment of the invention provides an aircraft-based control method and the aircraft. The aircraft comprises a fuselage, a nose, a tail and an aircraft control system. The nose with the propeller at the top end is rotatably connected with the front end of the fuselage in the plane direction of the central axis of the fuselage, wings are arranged on the two sides of the fuselage respectively,and rotors are arranged on the two sides of the tail respectively. The aircraft control system controls the flight attitude of the aircraft by acquiring the flight state information of the aircraft and controlling the rotation angle of the nose, the rotation of the propeller and/or the rotation of the two rotors at the tail of the aircraft according to the flight state information. According to the embodiment of the invention, the aircraft control system can control the operation state of the aircraft without controlling the pitch of the propeller, so that the control system is simple; meanwhile, the stability of the aircraft is improved through lift force generated by rotation of the propeller at the front end of the nose and/or force generated by rotation of the two rotor wings at the tail, so that the reliability of the aircraft is further improved.
本申请实施例提供一种基于飞行器的控制方法以及飞行器,该飞行器包括:机身、机头、机尾以及飞行器控制系统;顶端设置有螺旋桨的机头沿机身中轴线的平面方向可转动连接机身的前端,机身的两侧分别设置有机翼,机尾的两侧分别设置有旋翼。飞行器控制系统通过获取飞行器的飞行状态信息,并根据飞行状态信息控制机头的转动角度、螺旋桨的转动和/或机尾的两个旋翼的转动,以控制飞行器的飞行姿态。本申请实施例中飞行器控制系统无需控制螺旋桨的桨矩便可实现控制飞行器的运行状态,从而控制系统较简单;同时本申请中通过机头前端的螺旋桨转动所产生的升力和/或机尾的两个旋翼转动所产生的力来提高飞行器的稳定性,从而还提高了飞行器的可靠性。
Aircraft-based control method and aircraft
基于飞行器的控制方法以及飞行器
2020-10-13
Patent
Elektronische Ressource
Chinesisch
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