空中救护吊篮的自旋稳定

Chris Forden, Yanuel Trinidad, Ryan von Chance-Stutler, A. Bellocchio, James Bluman, M. Lanzerotti
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引用次数: 0

摘要

本文提出了一种稳定空中救护升降机吊篮旋转的新方法。直升机下冲产生的复杂力量可能会导致悬挂在救援担架上的病人剧烈旋转。在严重的情况下,旋转会使悬挂的载荷不稳定,有可能伤害病人,并危及机组人员的安全。所提出的设计采用了一个反扭矩装置来阻止旋转,这比标语更安全,更快,而且没有标语的战术限制。该装置遵循定制的控制规律,加速附着在垃圾上的飞轮,从而产生足够的角动量来抵消旋转并稳定悬浮的垃圾。惯性测量单元(IMU)测量垃圾的位置、角速度和角加速度,并将这些信息传递给微控制器。研究和原型设计是在美国陆军第160特种作战航空团(SOAR)的支持下开发的。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Spin Stabilization of an Air Ambulance Litter
This paper proposes a new approach to stabilize the spin of a suspended litter during air ambulance rescue hoist operations. Complex forces generated by the helicopter’s downwash may cause a patient suspended in a rescue litter to spin violently. In severe cases, the spin destabilizes the suspended load, risks injury to the patient, and jeopardizes the safety of the aircrew. The presented design employs an anti-torque device to arrest the spin that is safer and faster than a tagline and is without the tactical constraints of the tagline. The device follows tailored control laws to accelerate a flywheel attached to the litter, thereby generating sufficient angular momentum to counteract the spin and stabilize the suspended litter. An inertial measurement unit (IMU) measures the position, angular velocity, and angular acceleration of the litter and delivers this information to a microcontroller. The research and prototype design were developed under the support of the U.S. Army 160th Special Operations Aviation Regiment (SOAR).
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