摘要
根据四轴飞行器的结构和飞行模式,设计了系统的总体硬件电路结构。硬件电路基于Cortex—M4内核STM32F407系列ARM芯片。设计的外围电路包括无线通信模块、视频采集模块和GPS接收,发送模块以及测量飞行姿态的各个传感器模块。通过实验验证了所设计硬件电路系统的可行性。
Hardware circuit structure of the system is designed based on structure and flight mode of Quadrotor.The MCU of hardware circuit is based on Cortex-M4 STM32F4 series of ARM chips. The hardware circuit includes wireless communication module,video capture module and GPS receiving and transmitting module and each sensor modules which measure flight attitude. Feasibility of the designed hardware circuit system is validated by experiments.
作者
高明
张培亮
GAO Ming ZHANG Pei-liang(School of Optoelectronic Engineering, Xi' an Technological University, Xi' an 710021, China)
出处
《传感器与微系统》
CSCD
2017年第3期113-115,共3页
Transducer and Microsystem Technologies
基金
陕西省教育厅重点实验室科学研究计划项目(14JS034)