摘要
通过分析无人机飞行控制系统的工作原理以及对飞控计算机功能的需求,给出了基于ATmega128单片机的无人机飞行控制系统的硬件平台设计方法。本系统具有功能全、体积小、重量轻、功耗低、集成度高等特点,非常适合应用于小型无人机。
By analyzing the principle of UAV（ unmanned air vehicle） flight control system and the function requirement for flight control computer, the hardware platform design method of UAV＇ s flight control system based on the ATmega128 MCU is given. The whole system takes on characteristics of various of functions, small volume, little weight, low consumption and high integration, and it suits for applying to small UAV.
出处
《测控技术》
CSCD
2007年第2期44-46,49,共4页
Measurement & Control Technology
