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Adaptive Control of Variable-Pitch Propellers: Pursuing Minimum-Effort Operation

机译:可变螺距螺旋桨的自适应控制:追求最小努力

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As Unmanned Aerial Vehicles (UAVs) become more commonly used in industry, their performance will continue to be challenged. A performance bottleneck that is crucial to overcome is the design of electric propulsion systems for UAVs that operate in disparate flight modes (e.g., hovering and forward-moving flight). While flight mode dissimilarity presents a fundamental design challenge for fixed-geometry propulsion systems, variable-geometry systems such as the Variable Pitch Propeller (VPP) ones are able to provide superior propulsion performance across a wide range of flight modes. This work builds on previous work by the authors and presents a VPP system control and estimation framework for safe, nearminimum-electrical-effort propulsion system behavior across the whole operation state space of any UAV. Multiple simulated validations are presented to support the feasibility of the approach.
机译:随着无人驾驶飞机(UAV)在工业中的使用越来越普遍,其性能将继续受到挑战。克服关键的性能瓶颈是针对以不同飞行模式(例如,悬停和向前飞行)运行的无人机的电动推进系统的设计。尽管飞行模式的差异给固定几何推进系统带来了基本的设计挑战,但可变几何螺旋桨系统(VPP)等可变几何系统却能够在各种飞行模式下提供出色的推进性能。这项工作以作者先前的工作为基础,并提出了一个VPP系统控制和评估框架,用于在任何无人机的整个操作状态空间内实现安全,近乎最小的电力推动系统的行为。提出了多个模拟验证,以支持该方法的可行性。

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