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DYNAMICS SIMULATION AND CONTROL DESIGN OF GUN ADJUSTMENT FOR NONLINEAR MULTIBODY SYSTEM OF MULTIPLE LAUNCH ROCKET SYSTEM

机译:多管火箭炮系统非线性多体系统炮调整动力学仿真与控制设计

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The dynamics simulation of the processing of the gun adjustment for multiple launch rocket system (MLRS) as a complex nonlinear multibody system is studied. Based on the new version of transfer matrix method for multibody system (MSTMM), the nonlinear multibody system dynamics model of MLRS is established, and the overall transfer equation of the nonlinear multibody system is deduced. The launch dynamics simulation of MLRS is carried out by combining the general kinematics equations of rocket and Monte Carlo method, and the simulated results are verified by experiments. On this basis, the control design and dynamics simulation of the gun adjustment of MLRS has been preliminary studied by combing MSTMM with PD control method. The results show that the proposed control method has a good stability and can realize the automatic control of gun adjustment of MLRS quickly and accurately.
机译:研究了作为复杂非线性多体系统的多发火箭系统(MLRS)的火炮调整过程的动力学仿真。基于新版本的多体系统传递矩阵方法(MSTMM),建立了MLRS的非线性多体系统动力学模型,推导了非线性多体系统的整体传递方程。结合火箭的一般运动学方程和蒙特卡罗方法进行了MLRS的发射动力学仿真,并通过实验验证了仿真结果。在此基础上,结合MSTMM和PD控制方法,对MLRS的火炮调节控制设计和动力学仿真进行了初步研究。结果表明,所提出的控制方法具有良好的稳定性,可以快速,准确地实现MLRS机枪调整的自动控制。

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