小型无人机自动驾驶仪控制系统的研究

摘要

自动驾驶仪是无人机飞行控制系统的核心装置.本文设计的自动驾驶仪采用了两个处理器,且导航控制系统与姿态控制系统控制是分开的.它不仅具有高精度、高效率的性能,同时还具有通用性.文中对所设计的自动驾驶仪的结构和主要部件进行了介绍,同时着重分析了自主飞行模块.最后对飞行姿态进行仿真分析,仿真结果表明该系统满足性能要求.%Autopilot UAV is the core of the flight control system device.This paper used two processors for autopilot design, meanwhile navigation control system and attitude control system are controlled by separation.lt not only has high precision and efficiency, but also has generality .The paper introduced the design of the structure of autopilot and main components, and emphatically analysised the autonomous flight modules.At last flight attitude is used Simulation Analysis, simulation results show that the system meets the performance requirements.