论文部分内容阅读
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。
Ducted unmanned aerial vehicle is a new aircraft can take off and land vertically, the control system is its core component. Based on the demand of engineering application, a control system with high performance-price ratio, compact structure and low power consumption is designed for the ducted aircraft. The flight control strategy based on PID is proposed and the overall structure of control system, hardware and software are designed The system realizes the attitude and trajectory control of the aircraft and verifies the flight simulation test. The verification results show that the design scheme is reasonable and feasible and has high application value.