本设计是设计一个多旋翼倾转小型无人机，主要设计了无人机的硬件搭载部分和

This design is to design a multi-rotor tilting small UAV, which mainly designs the hardware and software control parts of the UAV, capable of straight-line lift, cruise, and aerial photography system. Because it is a tilt-rotor drone, it can be switched between the drone mode and the fixed-wing mode. It can generate lift by the rotor to make the drone take off and land vertically, or it can generate lift by the fixed wing, and the rotor generates thrust. Cruise. <br>The basic design, hardware selection, software system design of the UAV were carried out separately, and finally the overall design and optimization. At the same time, the physical model is established in Solidworks, the appropriate wing size is selected through the airfoil selection software, and the simple hardware control is performed through the code.

This design is to design a multi-rotor tilt small drone, mainly designed the hardware of the drone and software control part, can be straight up and down, cruise, equipped with aerial photography system and other functions. Because it is an tilt-rotor drone, it can be converted between the drone mode and the fixed-wing mode, both through the rotor to produce lift force allows the drone to take off and land vertically, but also through the fixed wing to produce lift, the rotor generates thrust to cruise.<br>The basic design, hardware selection and software system design of the uavor are carried out respectively, and the overall design and optimization are carried out. At the same time, solidworks to build a physical model, through the wing selection software to select the right wing size, through the code for simple hardware control and so on.

This design is to design a small multi rotor tilt UAV, mainly designed the hardware and software control part of the UAV, which can lift, cruise, and carry the aerial photography system. Because it is a tilt rotor UAV, it can switch between UAV mode and fixed wing mode. It can not only generate lift through the rotor to make the UAV take off and land vertically, but also generate lift through the fixed wing to generate thrust from the rotor to cruise.<br>The basic design, hardware selection and software system design of UAV are carried out respectively. Finally, the overall design and optimization are carried out. At the same time, the physical model is built in SolidWorks, the appropriate wing size is selected through the airfoil selection software, and the simple control of hardware is carried out through the code.