Some discussions about the error functions on SO(3) and SE(3) for the guidance of a UAV using the screw algebra theory

DOI10.1155/2017/1016530zbMath1353.93082OpenAlexW2568015724WikidataQ59142331 ScholiaQ59142331MaRDI QIDQ505963

Yong-Cai Geng, Sumit K. Garg

Publication date: 27 January 2017

Published in: Advances in Mathematical Physics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1155/2017/1016530

zbMATH Keywords

nonlinear differential equationsguidance3-dimensional special Euclidean group SE(3)6-DOF (Degree of Freedom) aircraft modeLie groups SO(3)screw algebra theoryunmanned aerial vehicle (UAV)

Mathematics Subject Classification ID

Related Items (1)

Geometric control using the state-dependent Riccati equation: application to aerial-acrobatic maneuvers

Cites Work

• Tube surfaces with type-2 Bishop frame of Weingarten types in E^3
• There is More than One Way to Frame a Curve
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