The Optimization Design about Flat Tail of Small Drones

Min Ji; Jing Feng He; Wei Ming Zhang

doi:10.4028/www.scientific.net/AMR.1030-1032.1260

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 1030-1032The Optimization Design about Flat Tail of Small...

The Optimization Design about Flat Tail of Small Drones

Abstract:

A multi-objective optimization method was advanced to make the drag and structure mass minimum of horizontal stabilizer based the precondition of meeting flying qualities. After the optimization, the longitudinal stability reduced, the longitudinal control performance increase. This method has referential meaning for the design of horizontal stabilizer for Mini-UVA.

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Periodical:

Advanced Materials Research (Volumes 1030-1032)

Pages:

1260-1263

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.1030-1032.1260

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Cite this paper

Online since:

September 2014

Authors:

Min Ji*, Jing Feng He, Wei Ming Zhang

Keywords:

Horizontal Stabilizer, Optimization Design, UVA

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* - Corresponding Author

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