TY - GEN
T1 - A fast method for generating aerodynamic data for missile trajectory simulation
AU - Chen, Han
AU - Wang, Shikun
AU - Deng, Hongbin
AU - Li, Kewei
AU - Li, Dongfang
AU - Wang, Chao
N1 - Publisher Copyright:
© 2017 IEEE.
PY - 2017/7/2
Y1 - 2017/7/2
N2 - The full-scale aerodynamic simulation of the missile has always been the first step in the overall design of the missile. After aerodynamic simulation, a large number of aerodynamic data for the missile are obtained, and the prerequisite for the missile trajectory simulation will be met. In this paper, some common data processing methods are used to identify the law of the aerodynamic parameters of the missile shape, so that all the aerodynamic parameters can be obtained by combining the interpolation algorithm with a small amount of aerodynamic parameters. This method greatly accelerates the Speed of the initial design of the missile, you can complete more design of the iterative optimization in a short period of time. Finally, the simulation results and the generated data were compared and the results were satisfactory.
AB - The full-scale aerodynamic simulation of the missile has always been the first step in the overall design of the missile. After aerodynamic simulation, a large number of aerodynamic data for the missile are obtained, and the prerequisite for the missile trajectory simulation will be met. In this paper, some common data processing methods are used to identify the law of the aerodynamic parameters of the missile shape, so that all the aerodynamic parameters can be obtained by combining the interpolation algorithm with a small amount of aerodynamic parameters. This method greatly accelerates the Speed of the initial design of the missile, you can complete more design of the iterative optimization in a short period of time. Finally, the simulation results and the generated data were compared and the results were satisfactory.
KW - Aerodynamic Data
KW - Parameter identification
KW - Trajectory simulation
UR - https://www.scopus.com/pages/publications/85050893094
U2 - 10.1109/ICUS.2017.8278345
DO - 10.1109/ICUS.2017.8278345
M3 - Conference contribution
AN - SCOPUS:85050893094
T3 - Proceedings of 2017 IEEE International Conference on Unmanned Systems, ICUS 2017
SP - 225
EP - 230
BT - Proceedings of 2017 IEEE International Conference on Unmanned Systems, ICUS 2017
A2 - Xu, Xin
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2017 IEEE International Conference on Unmanned Systems, ICUS 2017
Y2 - 27 October 2017 through 29 October 2017
ER -