The optimum theory and methods were adopted to design the laser beam riding guidance anti tank missile's control system in the short run. Through building the mathematical model of system, selecting a proper meth...The optimum theory and methods were adopted to design the laser beam riding guidance anti tank missile's control system in the short run. Through building the mathematical model of system, selecting a proper method and taking advantage of computer's high speed calculation and logic traits, an optimal controller was designed. Simulation results showed that the designed control system has fair performance and it satisfies the tactical and technical requirements. The results also demonstrate that by the combination of the optimizing methods and the computer the control system could be designed as soon as possible.展开更多
Determining characteristics of the initial fixed-focus are a key technique for the design of laser beam riding guidance missile. Through analyzing the effects of the initial cone information field in guidance and cont...Determining characteristics of the initial fixed-focus are a key technique for the design of laser beam riding guidance missile. Through analyzing the effects of the initial cone information field in guidance and control system of missile, those effects are considered as an approximate lead com- pensation network. The position and time of guidance spot initial fixed-focus can be designed. This method is applied to determine the characteristics of the initial fixed-focus of laser information field for a laser beam guidance gun-launched missile. The results of design and simulation show that the initial cone information field apparently speeds up convergence on the initial trajectory, and provides a guarantee for the implementation of minimum range index of a missile system.展开更多
为了解决激光驾束制导中发动机烟雾对制导激光场信号的衰减问题,采用van de Hulst近似计算方法,模拟研究了烟雾对1.06μm,1.55μm,10.6μm波长的激光在不同复折射率参量下的吸收、散射、衰减效应。结果表明,复折射率不变时,烟雾对长波...为了解决激光驾束制导中发动机烟雾对制导激光场信号的衰减问题,采用van de Hulst近似计算方法,模拟研究了烟雾对1.06μm,1.55μm,10.6μm波长的激光在不同复折射率参量下的吸收、散射、衰减效应。结果表明,复折射率不变时,烟雾对长波长激光的吸收衰减较小;烟雾对激光的衰减峰值随着折射率虚部的增大而变小;峰值的位置随着激光波长的增加向粒子半径增大的方向移动。该研究结果对激光驾束制导武器的研制具有较大的参考价值。展开更多
文摘The optimum theory and methods were adopted to design the laser beam riding guidance anti tank missile's control system in the short run. Through building the mathematical model of system, selecting a proper method and taking advantage of computer's high speed calculation and logic traits, an optimal controller was designed. Simulation results showed that the designed control system has fair performance and it satisfies the tactical and technical requirements. The results also demonstrate that by the combination of the optimizing methods and the computer the control system could be designed as soon as possible.
基金Supported by the Ministerial Level Foundation(62201070412)
文摘Determining characteristics of the initial fixed-focus are a key technique for the design of laser beam riding guidance missile. Through analyzing the effects of the initial cone information field in guidance and control system of missile, those effects are considered as an approximate lead com- pensation network. The position and time of guidance spot initial fixed-focus can be designed. This method is applied to determine the characteristics of the initial fixed-focus of laser information field for a laser beam guidance gun-launched missile. The results of design and simulation show that the initial cone information field apparently speeds up convergence on the initial trajectory, and provides a guarantee for the implementation of minimum range index of a missile system.
文摘为了解决激光驾束制导中发动机烟雾对制导激光场信号的衰减问题,采用van de Hulst近似计算方法,模拟研究了烟雾对1.06μm,1.55μm,10.6μm波长的激光在不同复折射率参量下的吸收、散射、衰减效应。结果表明,复折射率不变时,烟雾对长波长激光的吸收衰减较小;烟雾对激光的衰减峰值随着折射率虚部的增大而变小;峰值的位置随着激光波长的增加向粒子半径增大的方向移动。该研究结果对激光驾束制导武器的研制具有较大的参考价值。
