On 3D Path Following Control of a Ducted-Fan UAV on SO(3)

被引:0
|
作者
Cichella, Venanzio [1 ]
Naldi, Roberto [1 ]
Dobrokhodov, Vladimir [2 ]
Kaminer, Isaac [2 ]
Marconi, Lorenzo [1 ]
机构
[1] Univ Bologna, CASY DEIS, I-40133 Bologna, Italy
[2] Naval Postgradu Sch, Monterey, CA USA
关键词
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中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This article focuses on the problem of computing a control law for a particular class of tail-sitter aircraft able to switch their flight configuration from hover to level flight and vice-versa. We address the problem of steering a ducted-fan UAV along a given path (path following problem) so as to meet spatial constraints. One possible scenario is the situation where a vehicle is required to execute collision-free maneuvers under strict spatial limitations and arrive at his final destination while pointing with a camera to a moving target. Path following control in 3D builds on a nonlinear control strategy that is first derived at the kinematic level using the Special Orthogonal Group (SO(3)) theory.
引用
收藏
页码:3578 / 3583
页数:6
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