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Design of Missile Attitude Control System Based on Stochastic Robust Optimization

机译:基于随机稳健优化的导弹姿态控制系统设计

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? 2019, Editorial Board of Journal of Ballistics. All right reserved. ? 2019, Editorial Board of Journal of Ballistics. All right reserved. In order to solve the problem that the control system designed by multi-objective optimization algorithm is not robust,the missile attitude control system parameters were designed based on stochastic robust method,and the comparison simulation was carried out. Based on a determined structure of attitude control system,an index system including system stability,time domain index and frequency domain index items was proposed according to the requirements for rapidity and stability of the system. On this basis,the appropriate fitness functions were established respectively for the particle swarm optimization algorithm and the stochastic robust method via appropriate weighting for the indicators or the indicator dissatisfaction probabilities,and then the parameters of the attitude control system were optimized in the parameter value interval. Monte Carlo simulation experiments show the effectiveness of stochastic robust methods for the design of robust control system. In order to solve the problem that the control system designed by multi-objective optimization algorithm is not robust,the missile attitude control system parameters were designed based on stochastic robust method,and the comparison simulation was carried out. Based on a determined structure of attitude control system,an index system including system stability,time domain index and frequency domain index items was proposed according to the requirements for rapidity and stability of the system. On this basis,the appropriate fitness functions were established respectively for the particle swarm optimization algorithm and the stochastic robust method via appropriate weighting for the indicators or the indicator dissatisfaction probabilities,and then the parameters of the attitude control system were optimized in the parameter value interval. Monte Carlo simulation experiments show the effectiveness of stochastic robust methods for the design of robust control system.
机译:还2019年,弹道学杂志。保留所有权利。还2019年,弹道学杂志。保留所有权利。为了解决由多目标优化算法设计的控制系统不稳定的问题,基于随机稳健方法设计了导弹姿态控制系统参数,并进行了比较模拟。基于确定的姿态控制系统结构,根据系统的快速和稳定性的要求,提出了一种包括系统稳定性,时域指数和频域指数项目的指标系统。在此基础上,分别为粒子群优化算法和随机鲁棒方法通过适当加权来确定适当的健身功能,或者指示器不满概率,然后在参数值间隔中优化姿态控制系统的参数。蒙特卡罗仿真实验表明,随机控制系统设计的随机稳健方法的有效性。为了解决由多目标优化算法设计的控制系统不稳定的问题,基于随机稳健方法设计了导弹姿态控制系统参数,并进行了比较模拟。基于确定的姿态控制系统结构,根据系统的快速和稳定性的要求,提出了一种包括系统稳定性,时域指数和频域指数项目的指标系统。在此基础上,分别为粒子群优化算法和随机鲁棒方法通过适当加权来确定适当的健身功能,或者指示器不满概率,然后在参数值间隔中优化姿态控制系统的参数。蒙特卡罗仿真实验表明,随机控制系统设计的随机稳健方法的有效性。

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