首页> 外文会议>UAVs Eighteenth International Conference Mar 31-Apr 2, 2003 Bristol, United Kingdom >Attitude Control System for a Rotorcraft Micro Air Vehicle for Indoor Applications
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Attitude Control System for a Rotorcraft Micro Air Vehicle for Indoor Applications

机译:室内旋翼飞机微型飞行器的姿态控制系统

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The Division Microrobotics and Control Engineering of the University of Oldenburg is developing autonomous, electrically powered rotorcraft Micro Air Vehicles (MAVs) for indoor applications. The motivation for the development of these flying vehicles, which are up to 15 cm in size in any dimension, is their use as aerial superring assets for confined spaces (inside buildings, tunnels, stadiums, supermarkets etc). The strict limitation of airspace leads to the requirement of the ability to hover. This task is unlikely to be achieved by scaled-down conventional designs of fixed-wing aircraft in conjunction with forward thrust. Hence current research activities focus on wing-flapping and rotorcraft flight. This paper describes the design of a four-rotor mesoscopic helicopter, aerodynamic assessment and development of a subsystem for attitude determination and control with low-cost ac-celerometers.
机译:奥尔登堡大学微机器人与控制工程系正在开发适用于室内应用的自主式电动旋翼飞机微型飞行器(MAV)。开发这些飞行器的动机,这些飞行器的任何尺寸都长达15厘米,是它们被用作狭窄空间(建筑物,隧道,体育场,超级市场等)内的空中超级资产。空域的严格限制导致要求具有悬停能力。固定翼飞机按比例缩小的常规设计加上前推力不可能实现这一任务。因此,当前的研究活动集中于机翼拍打和旋翼飞机飞行。本文介绍了四旋翼中观直升飞机的设计,空气动力学评估以及使用低成本加速度计确定和控制姿态的子系统的开发。

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