Abstract
A system of carrier rockets tracing target points is modeled and simulated in Simulink platform of MATLAB, in order to reduce the workloads of designers in designing, analyzing, calculating and selecting the carrier rockets’ motion parameters. Based on the dynamic formula of carrier rockets strictly deduced in this study for tracing targets, a three-degree free tracing system simulation, combined with model simulation techniques, is established, and the proper carrier rockets’ design parameters are studied according to the results of the simulation. First, this paper introduces the background and stresses the importance of carrier rockets in national defense, and then analyzes the problems with system modeling and analysis to be solved. After designing some sub-system simulation modules and integrating them into Simulink platform, this research sets up an tracing simulation model. And finally, by executing the trascing system simulation under the condition of different guidance ratio values, this research obtains corresponding simulation results and compares the influences of various guidance ratio values on the tracing effects.
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References
Wang, Y., Chen, Q., Chang, S.: Visual simulation of six-degree free trajectory in multiple perspectives using Simulink and VRML. J. Weapon Equipment Eng. 40(01), 143–147 (2019)
He, J.: Simulation of missile guidance and control using Simulink. Sci. Educ. Guide (08), 32–33 (2017)
Gao, S.: Design of missile six-degree free trajectory simulation system based on MATLAB/Simulink. Sci. Technol. Eng. (1), 29–33 (2011)
Cai, H., Xiong, J., Zheng, G., Liu, H.: Simulation system of missile terminal guidance based on MATLAB. Inf. Syst. Eng. (03), 36–37 (2014)
Gao, H., Zhu, D., Zhang, H.: Research on missile simulation system based on Simulink. Sci. Technol. Innov. Appl. (19), 16–17 (2016)
Yang, Y., Tang, S.: Total trajectory simulation of sub missile based on Simulink. J. Syst. Simul. (06), 1442–1444+1449 (2006)
Cheng, Y., Jiang, D., Wang, R.: Dynamic simulation based on matlab/simulink of SAM guidance and control system. Control Technol. Tactical Missile (3), 9–13 (2003)
Zhang, K.: Six-degree free modeling and simulation of missile based on simulink. Shipboard Electron. Countermeasure 34(4), 72–76 (2011)
Geng, J., Chen, H., Cui, L.: Study on the calculation model of firing variables in the simulation modeling of surface to air missile. Naval Electron. Eng. 36(10), 87–89+114 (2016)
Xia, F., Zhao, Y.: Design of simulation system of surface to air missile based on HLA. J. Syst. Simul. (02), 296–299 (2007)
Wang, H., Wan, X., Yang, J., Zhao, J., Liu, C.: Research on visual simulation of ground to air missile tracing air target. J. Missiles Guidance 36(03), 22–24 (2016)
Liu, W., Li, X., Guan, Z., Shu, C.: Design and implementation of a general trajectory simulation system for surface to air missile. J. Projectiles Rockets Missiles Guidance 38(2), 35–38 (2018)
Li, Q.: Simulation Model Design and Implementation. Electronic Industry Press, Beijing (2010)
Lan, F.: Research and application of ground to air missile training simulation system. Practical Electron. (6), 39–39 (2015)
Zhang, D., Zhao, Y., Lei, H., Wu, Y.: Modeling and simulating on kinematic trajectory of ground-to-air missile controled by three-point method. Flight Dyn. 30(1), 57–60, 65 (2012)
Chen, J., Zhang, X., Zhang, G.: Research on launch dynamics modeling and simulating for surface-to-air missile. J. Projectiles Rockets Missiles Guidance 30(1), 65–67, 71 (2010)
Zhou, L., Zhao, J., Lou, S.: Research into the trajectory simulation model of ground to air missile. Fire Control Command Control 31(10), 69–72 (2006)
Ou, J., Li, G., Gao, Z.: Three-dimensional trajectory simulation of air defense missile based on matlab. Fire Control Command Control 35(2), 166–168 (2010)
Wang, J., Zhou, L., Lei, H.: Forecast model and arithmetic on hit point of ground-to-air missile and aerial target. J. Syst. Simul. 21(1), 80–83 (2009)
Gao, H., Zhang, H., Kong, F.: Research of missile system. Defense Manuf. Technol. Simul. Simulink (2), 67–72 (2016)
Zhang, Z., Tong, Y., Zhang, W.: Research on the proportional guidance trajectory simulation. Tactical Missile Technol. (2), 56–59 (2005)
Qiang, S., Yi, D., Tu, X.:Simulation research on tracing of tactical trajectory missile. J. Trajectorys (03), 34–37 (2007)
Wang, Y., Xu, C., Zheng, X., Sun, G., Jian, Y.: Initial proportional guidance method with fall angle constraint and overload constraint. J. Projectile Guidance 39(04), 29–32+36 (2019)
Wang, P., Liu, H., Zou, H.: Research on simulation about the miss distance of the portable surface-to-air missile. Ship Electron. Eng. 31(6), 108–110 (2011)
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© 2021 ICST Institute for Computer Sciences, Social Informatics and Telecommunications Engineering
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Li, P., Zhu, Z., Chen, H., Li, S. (2021). Motion Simulation of Rocket Based on Simulink. In: Song, H., Jiang, D. (eds) Simulation Tools and Techniques. SIMUtools 2020. Lecture Notes of the Institute for Computer Sciences, Social Informatics and Telecommunications Engineering, vol 370. Springer, Cham. https://doi.org/10.1007/978-3-030-72795-6_43
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DOI: https://doi.org/10.1007/978-3-030-72795-6_43
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