Dynamics Modeling of Main Rotor Teeterboard Flap on Unmanned Autonomous Rotorcraft by D' Alembert Principle

Cun Guang Fang; Jie Li; Wei Wang

doi:10.4028/www.scientific.net/AMR.476-478.969

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 476-478Dynamics Modeling of Main Rotor Teeterboard Flap...

Dynamics Modeling of Main Rotor Teeterboard Flap on Unmanned Autonomous Rotorcraft by D' Alembert Principle

Abstract:

On teeterboard flap of main rotor rotating around free space point of a 30Kg class unmanned autonomous helicopter (UAH), aerodynamics kinematics model is set up in terms of D' Alembert principle. On conditions of the helicopter physical parameter value, simulation validates the model in reason, and points out：①Teeterboard Flap on main rotor is self-stable system; ②unmanned autonomous helicopter structure plays a leading role on transient process of main rotor teeterboard flap, and relative air current acting on the blade plays a leading role on its steady process.

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Periodical:

Advanced Materials Research (Volumes 476-478)

Pages:

969-973

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.476-478.969

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Online since:

February 2012

Authors:

Cun Guang Fang, Jie Li, Wei Wang

Keywords:

Modeling Based on D'Alembert Principle, Teeterboard Flap, Unmanned Autonomous Helicopter

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References

[1] WANG Shicun, Helicopter aerodynamics, Nanjing aviation college press, Nanjing, 1985 ( In Chinese )

Google Scholar

[2] Turnour Sr, Celi R. Modeling of flexible rotor blades for helicopter flight dynamics applica- tions[J], J. American Helicopter Society, 41,( 1996 )52-66

DOI: 10.4050/jahs.41.52

Google Scholar

[3] Schlichting H，Truckenbrodt E, Aeroplane aerodynamics, National defense industry press，Beijing, (1978)

Google Scholar

[4] Theoretical mechanics teaching and research group, Harbin Institute of Technology, Theoretical mechanics, Higher education press, Beijing, 1997 ( In Chinese ).

Google Scholar

[5] Bemporad A,Giorgetti N, A logic-based hybrid solver for optimal control of hybrid systems, Pro. 42nd IEEE Conference on Decision and Control, Maui, 2003, pp.640-645

DOI: 10.1109/cdc.2003.1272636

Google Scholar