Affiliation:
1. College of Mechanica Engineering, North University of China, Taiyuan 030051, China
Abstract
This paper presents a servo control method for the multiple launch rocket system (MLRS) launcher during marching fire operations. The MLRS, being a complex nonlinear system, presents challenges in designing its servo controller. To address this, we introduce the fuzzy adaptive sliding mode control (FASMC) approach. The permanent magnet synchronous motor (PMSM) and controller of the MLRS were simulated in the MATLAB/Simulink environment. The dynamic model of the MLRS during marching fire was established using multi-body system theory, vehicle mechanics, and launch dynamics. The dynamic model was then integrated with the FASMC-based controller using the Adams/View module. Numerical calculations were performed to demonstrate the control performance and the effectiveness and applicability of the proposed approach were validated through a comparison experiment between FASMC and other common control methods.
Funder
National Defense Pre-Research Foundation of China
Subject
Electrical and Electronic Engineering,Industrial and Manufacturing Engineering,Control and Optimization,Mechanical Engineering,Computer Science (miscellaneous),Control and Systems Engineering
Reference39 articles.
1. Rui, X.T., Lu, Y., Wang, G., Chen, W., and Yun, L. (2003). Simulation and Test Methods of Launch Dynamics of Multiple Launch Rocket System, National Defence Industry Press.
2. The impact of launcher turret vibrations control on the rocket launch;Dziopa;Bull. Pol. Acad. Sci. Tech. Sci.,2015
3. A simplified dynamic model and control for a multiple launch rocket system;Li;J. Vib. Control,2021
4. Neural-network-predictor-based control for an uncertain multiple launch rocket system with actuator delay;Li;Mech. Syst. Signal Process.,2020
5. On Modeling and Dynamics of a Multiple Launch Rocket System;Li;Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng.,2021
Cited by
1 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献