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Icing detection and identification for unmanned aerial vehicles using adaptive nested multiple models

机译:基于自适应嵌套多模型的无人机结冰检测与识别

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摘要

A multiple-model approach for icing diagnosis and identification in small unmanned aerial vehicles is proposed. The accretion of ice layers on wings and control surfaces modifies the shape of the aircraft and, consequently, alters the performance and controllability of the vehicle. Pitot tubes might be blocked due to icing, providing errors in the airspeed measurements. In this paper, we propose a nested multiple-model adaptive estimation framework to detect and estimate icing using standard sensors only, ie, a pitot tube and an inertial measurement unit. The architecture of the estimation scheme is based on 2 different time scales, ie, one for the accretion of ice on aircraft surfaces and one for the accretion of ice on sensors, and consists of 2 nested adaptive observers, namely, outer and inner loops, respectively. The case study of a typical small unmanned aerial vehicle supports and validates the proposed theoretical results.
机译:提出了一种小型无人机结冰诊断和识别的多模型方法。机翼和控制表面上积聚的冰层改变了飞机的形状,因此改变了车辆的性能和可控性。皮托管可能会因结冰而阻塞,从而在空速测量中产生误差。在本文中,我们提出了一个嵌套的多模型自适应估计框架,仅使用标准传感器即皮托管和惯性测量单元来检测和估计结冰。估算方案的架构基于2个不同的时间尺度,即一个用于在飞机表面上积冰,另一个用于在传感器上积冰,并且由2个嵌套的自适应观测器组成,即外圈和内圈,分别。一个典型的小型无人机的案例研究支持并验证了所提出的理论结果。

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