无人直升机自动起飞控制技术研究  

Research on Automatic Takeoff Control Technology for Unmanned Helicopter

作　　者：丁锐[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：《计算机测量与控制》2007年第11期1506-1508,1522,共4页Computer Measurement &Control

摘　　要：以无人直升机起飞段非线性模型为对象,研究了自动起飞控制技术方案,以空中定点控制方案为起点根据控制仿真结果对系统进行改进控制,分别加入线加速度反馈和直接力反馈,达到较好的无人直升机自动起飞控制要求。This paper takes the non-linear model of unmanned helicopter takeoff as the object, has studied out the technology project of automatic takeoff control, the project of air fixed-point control is set as the start point, according to the control emulation result the control of system is improved, the feedback of lineaer acceleration and direct force are added respectively, to achieve the better automatic takeoff control demand of the unmanned helicopter.

关 键 词：无人直升机 定点控制 自动起飞 线加速度 直接力 

分 类 号：TP273[自动化与计算机技术—检测技术与自动化装置] V279[自动化与计算机技术—控制科学与工程]