Modeling and Hovering Control of an Ducted-Fan UAV in Low Speed Crosswind

Hong Lei An; Jian Wen Wang; Jian Wang; Hong Xu Ma

doi:10.4028/www.scientific.net/AMR.466-467.1060

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 466-467Modeling and Hovering Control of an Ducted-Fan UAV...

Modeling and Hovering Control of an Ducted-Fan UAV in Low Speed Crosswind

Abstract:

National University of Defense Technology has begun a research program to investigate and test ducted-fan propeller architecture for UAV designing. Development of a prototype continues to support ongoing research in the area of autonomous systems. In this paper, we build a nonlinear dynamic model of Ducted-Fan UAV for verifying appropriate controller behavior, and design a hierarchical controller for hovering flight of the UAV.

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Periodical:

Advanced Materials Research (Volumes 466-467)

Pages:

1060-1064

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.466-467.1060

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Online since:

February 2012

Authors:

Hong Lei An, Jian Wen Wang, Jian Wang, Hong Xu Ma

Keywords:

Ducted-Fan UAV, Hovering Control, Modeling

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References

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