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

被引:0
|
作者
Henderson, Travis [1 ]
Papanikolopoulos, Nikolaos [1 ]
机构
[1] Univ Minnesota, Dept Comp Sci & Engn, Minneapolis, MN 55455 USA
基金
美国国家科学基金会;
关键词
UAV; INSPECTION;
D O I
10.1109/icra40945.2020.9197208
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
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, near-minimum-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.
引用
收藏
页码:7470 / 7476
页数:7
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