无人直升机飞行控制系统的设计与实现  

The design and realization of flight control system for unmanned helicopter

作　　者：孙雪[1] 安敬蕊[1] 

机构地区：[1]南京航空航天大学自动化学院,江苏南京210016

出　　处：《电子设计工程》2013年第20期91-93,共3页Electronic Design Engineering

摘　　要：针对某型无人直升机的性能要求,以某型无人直升机为背景,本文设计了基于DSP28335的飞控系统。本文首先介绍了设计的总体方案、各分系统设计思想及其软硬件实现,最后通过进行半物理仿真试验得出试验结果。试验结果表明该飞控系统设计合理,满足无人直升机的性能要求,具有一定的工程实用价值。In order to meet the performance requirements of unmanned helicopter, the paper presents a flight control system based on a type unmanned aerial vehicle. Firstly introduce the overall design scheme and the hardware, software realization of main subsystems. Lastly, carry out the semi-physical simulation and get the result. The result shows that the design of the flight control system is reasonable and it satisfies the performance requirements of the unmanned helicopter and further engineering applications.

关 键 词：无人直升机 飞控系统 DSP微处理器 半物理仿真 

分 类 号：TN98[电子电信—信息与通信工程]