Abstract
The modeling of aircraft motion is very important for aircraft flight performance evaluation, aero-engine design and air-combat modeling and simulation. However, the flight of aircraft is a complex process, and its flight capability is affected by many factors. The existing modeling process is generally based on analytic methods or energy methods, which leads to complex modeling process or lower model accuracy. For this reason, we deduced the coordinate transformation matrix, and on this basis, established a differential equation of aircraft motion with the earth fixed axis system, and finally built an aircraft motion model based on the numerical integration method. Experiments show that the method is simple and high-precision, and can meet the requirements of rapid modeling of warfare simulation.
This is a preview of subscription content, log in via an institution to check access.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Feng, Z., Yiping, Y., Wenjie, T., et al.: A high performance framework for modeling and simulation of large-scale complex systems. Future Gener. Comput. Syst. 2015(51), 132–141 (2015)
Rolfe, J.M., Staples, K.J.: Flight simulation, pp. 56–89. Cambridge University Press, Cambridge (1986)
Li, X., Xing, X.: Design & implementation of civil transport takeoff performance program. J. Civil Aviat. Univ. China 26(1), 8–13 (2008)
Wang, L., Jia, L.: Simulation of aircraft flight system based on motion differential equation. J. China Civil Aviat. Univ. 23(zl), 82–85 (2005)
Hua, Z.: Research on aircraft engine modeling for flight simulation. Nanjing University of Aeronautics and Astronautics (2010)
Gu, H.: Dynamic model of aircraft ground handling. Acta Aeronautica et Astronautica Sinica 22(2) (2001)
Shui, Q.-C., Wang, Q.-H.: A mathematical model used to calculate the takeoff performance for an aircraft. Flight Dyn. 19(4), 70–74 (2001)
Wang, J.: Improvement to quaternion-based model of rigid aircraft motion. J. Syst. Simul. 18(2), 230–232 (2006)
Gai, Y., Gu, W., Xu, Y., Li, C.: A method for designing mobile capability simulation system of avion. Comput. Simul. 26(1), 87–102 (2009)
Fang, Z.: Aircraft Flight Dynamics, p. 6. Beijing University of Aeronautics and Astronautics Press, Beijing (2005)
Johnson, S.A.: A simple dynamic engine model for use in a real-time aircraft simulation with thrust vectoring. NASA Technical Memorandum, vol. 4240 (1990)
Author information
Authors and Affiliations
Corresponding authors
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2017 Springer Nature Singapore Pte Ltd.
About this paper
Cite this paper
Zhang, M., Yao, Y. (2017). Aircraft Motion Model Based on Numerical Integration. In: Mohamed Ali, M., Wahid, H., Mohd Subha, N., Sahlan, S., Md. Yunus, M., Wahap, A. (eds) Modeling, Design and Simulation of Systems. AsiaSim 2017. Communications in Computer and Information Science, vol 751. Springer, Singapore. https://doi.org/10.1007/978-981-10-6463-0_44
Download citation
DOI: https://doi.org/10.1007/978-981-10-6463-0_44
Published:
Publisher Name: Springer, Singapore
Print ISBN: 978-981-10-6462-3
Online ISBN: 978-981-10-6463-0
eBook Packages: Computer ScienceComputer Science (R0)