Research Article
Motion Simulation of Rocket Based on Simulink
@INPROCEEDINGS{10.1007/978-3-030-72795-6_43, author={Pengcheng Li and Zhi Zhu and Haidong Chen and Shipeng Li}, title={Motion Simulation of Rocket Based on Simulink}, proceedings={Simulation Tools and Techniques. 12th EAI International Conference, SIMUtools 2020, Guiyang, China, August 28-29, 2020, Proceedings, Part II}, proceedings_a={SIMUTOOLS PART 2}, year={2021}, month={4}, keywords={Rockets Simulation Simulink Proportion guidance}, doi={10.1007/978-3-030-72795-6_43} }- Pengcheng Li
Zhi Zhu
Haidong Chen
Shipeng Li
Year: 2021
Motion Simulation of Rocket Based on Simulink
SIMUTOOLS PART 2
Springer
DOI: 10.1007/978-3-030-72795-6_43
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.
