Helicopter Aerodynamic Parameter Identification via Flight Dynamics

Xue Mei Yu; An Ping Zhao; Xue Li

doi:10.4028/www.scientific.net/AMM.327.246

Paper Titles

Review of Coupled Research for Mechanical Dynamics and Fluid Mechanics of Reciprocating Compressor
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Study on Theoretical Mechanics with Mechanics Properties in Exercise Class
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Study of Interfacial Stiffness by Using the Structural Interface Model Based on Elastic Mechanics
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Helicopter Aerodynamic Parameter Identification via Flight Dynamics
p.246

Simulation on Computational Fluid Dynamics of Flow Field and Pollutant Dispersion in Block of Buildings
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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 327Helicopter Aerodynamic Parameter Identification...

Helicopter Aerodynamic Parameter Identification via Flight Dynamics

Abstract:

A method which can process flight test data by integrating parameter identification and non-dimensional flight dynamic model was proposed to acquire the effective aerodynamic parameters of a helicopter. First of all, a non-dimensional mathematic model considering flight dynamics was deduced for a helicopter in state of level flight, and some important parameters including aerodynamic and correctional were developed. Next, taking helicopter Z-9× for example, the least squares method was adopted to identify these parameters based actual flight test data. Lastly, the identification method was proved valid through feasibility analysis. Results show that this method is a good way to acquire aerodynamic parameters and can shorten flight test periods as well.

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Periodical:

Applied Mechanics and Materials (Volume 327)

Pages:

246-249

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.327.246

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Online since:

June 2013

Authors:

Xue Mei Yu, An Ping Zhao, Xue Li

Keywords:

Aerodynamic Parameter, Feasibility Analysis, Flight Dynamics, Parameter Identification

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References

[1] K W. Cliff. Aircraft Parameter Estimation-AIAA Dryden lecture in Research for 1987. NASA TM-88281

Google Scholar

[2] P. Hamel. Rotorcraft system identification: AGARD LS-178 (1991), pp.332-337

Google Scholar

[3] S. Kirschstein, W. Alles. Parameter identification with a controlled free flying model of a space plane: Aerospace Science and Technology, Vol.9, No.4 (2005), pp.348-356.

DOI: 10.1016/j.ast.2005.03.001

Google Scholar

[4] I. Mitsuaki, N. Masatoshi and N. Kazuhide. Nonlinear adaptive model following control for a 3-DOF tandem-rotor model helicopter: Control Engineering Practice, Vol.18 (2010), pp.936-943

DOI: 10.1016/j.conengprac.2010.03.017

Google Scholar

[5] D. J. Wu, P. Li. A modeling method of miniature unmanned helicopter based on parameter identification: Acta Aeronautica et Astronautica Sinica, Vol.28, No.4 (2007), pp.845-850 (in Chinese)

Google Scholar

[6] Y. Z. Tang: Helicopter Control System Design.( Defense Industry Press, Beijing 2000) (in Chinese)

Google Scholar

[7] X. M. Yu, P.A. Liu, X. J. Cui. Helicopter's hovering performance expanded by using the parameter identification method. Acta Aeronautica Et Astronautica Sinica, Vol.31, No.3 (2010), pp.466-471 (in Chinese)

Google Scholar

[8] R. L. Chen, X. M. Yu, et al. Helicopter Aerodynamic Parameter Identification in Vertical Flight. Acta Aerodynamica Sinica, Vol.24, No.1 (2006), pp.115-119 (in Chinese)

Google Scholar