Takeoff and landing control using force sensor by electrically-powered helicopters
Takeoff and landing control using force sensor by electrically-powered helicopters
复制标题
电动直升机使用力传感器进行起飞和着陆控制
DOI：
10.1109/amc.2006.1631633
复制
发表时间：
2006
期刊：
影响因子：
--
通讯作者：
M. Fujita
中科院分区：
文献类型：
--
作者：
A. Shimada;M. Fujita
介绍了一种利用力传感器控制直升机起降的方法。该系统包括一架小型电动直升机，一个飞行基地，在飞行基地下设置力传感器，和一个直升机控制终端，连接到一个系统控制器。当直升机停在基座上时，力传感器输出与直升机重量相对应的数据。当工作电压上升时，直升机几乎从基地起飞。同时，力传感器输出接近于0。这意味着与力输出相关的升力从0 N变为与重量对应的值。本文介绍了系统的设计过程，包括系统建模和实验结果
A takeoff and landing control of helicopters using a force sensor helicopter is introduced. The system consists of a small electrically-powered helicopter, a flight base under which the force sensor is set, and a helicopter control terminal which is connected to a system controller. When the helicopter stands on the base, the force sensor outputs data corresponding to the weight of the helicopter. As the operational voltage rises, the helicopter almost takes off from the base. Concurrently, the force sensor output closes to 0. It means that lift force related to force output becomes from 0 N to the value corresponding to the weight. This paper introduces the design process including system modeling and the experimental results