Control and Limitations of Navigating a Tail Rotor/Actuator Failed Unmanned Helicopter
Control and Limitations of Navigating a Tail Rotor/Actuator Failed Unmanned Helicopter
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DOI：
10.1007/s10846-010-9512-x
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发表时间：
2011
影响因子：
3.3
通讯作者：
Richard Garcia;Ainsmar Brown
中科院分区：
文献类型：
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作者：
Richard Garcia;Ainsmar Brown
根据美国联邦航空管理局（FAA）关于机械故障的统计数据，尾桨故障是直升机致命事故的第三大原因。尾桨故障对人员和任务目标构成严重危害，并可能造成高额的财政损失。这对于无人直升机来说尤其如此，它不能配备载人直升机上的故障安全标准。这项工作提供了一个概述如何直升机可以控制后尾桨故障及其适用于载人和无人驾驶车辆。这项工作特别详细说明了这种类型的软件故障控制的一些限制。
According to Federal Aviation Administration (FAA) statistics on mechanical failures, tail rotor failure is the third highest cause of fatal accidents in helicopters. Tail rotor failure represents a serious hazard to personnel and mission objectives and can create high fiscal loss. This is especially true for unmanned helicopters, which cannot be equipped with the fail-safes standard on manned counterparts. This work provides an overview of how a helicopter can be controlled after a tail rotor failure and its applicability to both manned and unmanned vehicles. This work specifically details some of the limitations of this type of software failure control.