Dynamic Analysis Helicopter Flight Simulator

Article Preview

Abstract:

For helicopter structural characteristics, this article focuses on the helicopter to take off, hover and other state aerodynamic analysis, the establishment of the fuselage-landing gear dynamics model; while the helicopter simulator simulation system are described, and the kinetic model was built simulation analysis, simulation results and the actual flight conditions consistent, indicating that the model is correct, there is a certain reference value.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

1305-1308

Citation:

Online since:

March 2014

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2014 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] GK. Taylor, A.L.R. Thomas. Animal flight dynamics ii. Longitudinal stability in flapping flight [J]. Journal of Theoretical Biology, 2002, 214(3): 351-370.

DOI: 10.1006/jtbi.2001.2470

Google Scholar

[2] Pratumnopharat R, Leung P. S. Validation of various windmill brake state models used by blade element momentum calculation[J]. Renewable Energy, 2011, 36(11): 3222-3227.

DOI: 10.1016/j.renene.2011.03.027

Google Scholar

[3] Zhu Zheng-hong, Larosa Michael, Ma James. Fatigue life estimation of helicopter landing probe based on dynamic simulation [J]. Journal of Aircraft, 2009, 46(5): 1544-1544.

DOI: 10.2514/1.38345

Google Scholar

[4] Huang Xingli, Zhu, Jihong Liu, Shiqian. Neural network adaptive control for small unmanned tandem helicopter [J]. Sixth World Congress on Intelligent Control and Automation, 2006, 1: 9302-9306.

DOI: 10.1109/wcica.2006.1713801

Google Scholar

[5] Shih CL, Chen ML, Wang JW. Mathematical model and set-point stabilizing controller design of a twin rotormimo system[J]. Asian journal of control, 2008, 10(1): 107-114.

DOI: 10.1002/asjc.11

Google Scholar