Virtual Flight Modeling and Simulation of Air-launched Anti-ship Missile

Authors

Zhipeng Sun, School of Automation Science and Electrical Engineering, Beihang University, Beijing 100083, China;
Guanghong Gong, School of Automation Science and Electrical Engineering, Beihang University, Beijing 100083, China;

Abstract

Abstract: The relationship between the parameters affecting aerodynamic force was studied, and the aerodynamic coefficient was properly linearly simplified. According to the type of airborne anti-ship missile performance model, the "black box modeling" and extrapolation method was adopted to determine its aerodynamic coefficient, a typical anti-ship missile six degrees of freedom of the simplified dynamic model was established. By studying the flight phases after the missile launch, the flight trajectory model of each flight phase was established by using the control method of the track angle. The whole flight trajectory process of the missile attacking a target was realized and the simulation results of the flight path were obtained, which would provide missile attack model support for air defense and anti-missile of surface ship in virtual countermeasure simulation system.

Recommended Citation

Sun, Zhipeng and Gong, Guanghong (2020) "Virtual Flight Modeling and Simulation of Air-launched Anti-ship Missile," Journal of System Simulation: Vol. 29: Iss. 10, Article 42.
DOI: 10.16182/j.issn1004731x.joss.201710042
Available at: https://dc-china-simulation.researchcommons.org/journal/vol29/iss10/42

First Page

2567

DOI Link

https://doi.org/10.16182/j.issn1004731x.joss.201710042

Last Page

2573

CLC

V411.8

Recommended Citation

Sun Zhipeng, Gong Guanghong. Virtual Flight Modeling and Simulation of Air-launched Anti-ship Missile[J]. Journal of System Simulation, 2017, 29(10): 2567-2573.

DOI

10.16182/j.issn1004731x.joss.201710042