某型涵道无人飞行器控制系统设计

涵道无人飞行器是一种可垂直起降的新型航空器,控制系统是其核心组成部分.从工程应用需求出发,针对涵道飞行器设计了一种具有高性能价格比、结构紧凑、低功耗的控制系统;提出基于PID的飞行控制策略并给出了控制系统总体结构,设计硬件与软件系统实现飞行器的姿态和轨迹控制,并进行飞行仿真试验验证.验证结果表明,设计方案合理可行,具有很高的应用价值.

Control System of Ducted Fun UAV

The ducted fun UAV(Unmanned Aerial Vehicle) is a vertical take-off and landing(VTOL) aircraft.The control system is the key component of the ducted fun.From the engineering application requirements,a control system with high performance-price ratio,compact structure and low-power consumption is designed and implemented for the ducted aircraft.The control strategy and the overall structure of the control system are introduced.The hardware and software system are designed to realize attitude and trajectory control and flight simulation experimental test is taken.The experiment results indicate that the solution is correct and workable.