基于C8051F040单片机的无人机飞控系统软件模块化设计  

A Modularized Software Design for UAV's Flight Control System Based on C8051F040

作　　者：云超[1] 路平[1] 甄云卉[1] 

机构地区：[1]军械工程学院光学与电子工程系,石家庄050003

出　　处：《科学技术与工程》2010年第4期1045-1048,共4页Science Technology and Engineering

摘　　要：针对某型无人机的飞控系统,在飞控机硬件设计基础上设计了机载飞控软件。由于硬件设计充分考虑了自检功能,故采用软件判别,能判定飞控机及部分电路是否正常工作。例如,舵机控制电路输出的电压信号,都由A/D采集下来,通过进行比较判别,就可知道该电路是否有故障。An airborne flight control software is designed for a certain UAV flight control system based on hardware of UAV. Because of the hardware take into acconnt the function of self check-up, so it judge by software, which can judge whether or not the circuit can be worked normally. For example, the output of pressure by the servo which collect by AD. Comparison, can know whether the circuit have malfunction.

关 键 词：无人机 飞控计算机 C8051F040 模块化软件 

分 类 号：TP311.52[自动化与计算机技术—计算机软件与理论] V279[自动化与计算机技术—计算机科学与技术]