A Type of Fighter Dynamics Modeling and Simulation

Ding Xuan Zhao; Ying Jie Li; Guo Jun Yang; Qing Bo Hao; Gang Liu; Miao Xu

doi:10.4028/www.scientific.net/AMR.466-467.577

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 466-467A Type of Fighter Dynamics Modeling and Simulation

A Type of Fighter Dynamics Modeling and Simulation

Abstract:

Dynamics model of fighter was proposed in order to drive on flight simulator virtually. The model took Lagrange equation as basis and simplified analysis of the force on fighter according to the real-time input state information from joystick. The dynamics equation was solved in real time using Runge-Kutta method (RK4). It was proved finally that the model and simulation algorithm had higher dependability through datum and simulation scene which was obtained with graphics engine OpenGVS and 3D visual modeling Software Multigen Creator.

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Periodical:

Advanced Materials Research (Volumes 466-467)

Pages:

577-581

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.466-467.577

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Online since:

February 2012

Authors:

Ding Xuan Zhao, Ying Jie Li, Guo Jun Yang, Qing Bo Hao, Gang Liu, Miao Xu

Keywords:

Dynamics Model, Fighter, Lagrange Equation, Runge-Kutta Method, Simulation

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References

[1] C C Sui, Y T Yang and R Z Jia: Flight Dynamics, vol. 21(2003) No. 3, p.59–60.

Google Scholar

[2] S J Zou, M Q Hu and J L Li: Journal of Air Force Engineering University, vol. 6(2005) No. 6, p.10–12.

Google Scholar

[3] W L Fang and X K Shen: Journal of Zhejiang University-Science C, vol. 11(2010) No. 11, p.911–918.

Google Scholar

[4] N. Ravenel, J.F. Artaud and S. Bremond: Fusion Engineering and Design, vol. 85(2008) No. 6, p.482–486.

Google Scholar

[5] G. Tarantino, C. Fazio and R.M. Sperande-Mineo: Computer Applications in Engineering Education, vol. 18(2010) No. 3, p.144–156.

Google Scholar

[6] X L Zheng and S Tang: CAR 2010-2010 2nd International Asia Conference on Informatics in Control, Automation and Robotics(China, August, 2010). Vol. 3, p.242–245.

DOI: 10.1109/car.2010.5456740

Google Scholar

[7] S. Ch. Palligkinis and G. Papageorgiou: Applied Mathematics and Computation, vol. 209(2009) No. 3, p.97–105.

Google Scholar