摘要
设计了一种微型飞行器飞行稳定控制系统,该系统以STM32单片机为主控,实时检测微型飞行器飞行过程中的俯仰角、航向角、横滚角等飞行参数,通过飞行控制、姿态测量、通信传输和控制显示等模块数据交联,确定其准确姿态和位置,可实现飞行的精准控制和定点巡航功能,并保证飞行器的安全可靠。此研究在一定程度上可促进微型飞行器在军事民用等领域的应用。
In this paper,we design an MAV（ Micro Air Vehicle） flight stability control system. The control system,with STM32 MCU as the master,can detect parameters such as pitching angle,course angle,roll angle in the real-time in the process of MAV flight,through cross linking of data of modules,the flight control,attitude measurement,communication transmission can be carried out and displayed,its posture and position are determined accurately,the precise control of flight and function of fixed-point cruise are realized,and the safe and reliability in the process of aircraft in flight are ensured. The study can promote the MAV applications in military and civil fields.
出处
《实验室研究与探索》
CAS
北大核心
2015年第7期122-124,共3页
Research and Exploration In Laboratory
基金
国家"本科教学工程"本科专业综合改革试点建设项目(ZG0296)
国家"本科教学工程"大学生校外实践教育基地建设项目(284)
滨州学院科研基金项目(BZXYG1320)
滨州学院实验技术研究重点项目(BZXYSYXM201302
BZXYSYXM201401)
