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Optimum Design of the Control System for a Laser Beam Riding Guidance Anti-Tank Missile 被引量:3
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作者 翁彦 王正杰 张天桥 《Journal of Beijing Institute of Technology》 EI CAS 2000年第2期160-165,共6页
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
关键词 laser beam riding guidance anti-tank missile control system optimizing method
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Determining the characteristics of the initial fixed-focus of laser beam riding guidance information field
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作者 梅跃松 于剑桥 +1 位作者 于天朋 李景须 《Journal of Beijing Institute of Technology》 EI CAS 2013年第1期6-11,共6页
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
关键词 laser beam riding guidance laser information field lead-in trajectory missile guidanceand control system gun-launched missile
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Simulation Study on the Feasibility of Gun-Launched Missile Against Attack Helicopters
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作者 王狂飙 张天桥 《Journal of Beijing Institute of Technology》 EI CAS 2001年第1期75-80,共6页
The feasibility of providing the tank a limited anti helicopter ability with gun launched missile is studied. A type of simulation model of gun launched missile against attack helicopters is established. The simula... The feasibility of providing the tank a limited anti helicopter ability with gun launched missile is studied. A type of simulation model of gun launched missile against attack helicopters is established. The simulation and the parameter optimization of missile control system under various circumstances are done. The gun launched missile can directly hit the helicopters in the typical tracks, all the missdistances are less than 1?m and the maximum overload is less than available overload. Gun launched missile is a feasible choice for tanks against attack helicopters. 展开更多
关键词 gun launched missile attack helicopters rolling missile beam riding guidance simulaion control system
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