期刊文献+
共找到3篇文章
< 1 >
每页显示 20 50 100
反弹道导弹动能拦截器的新型最优制导律 被引量:3
1
作者 李振营 沈毅 胡恒章 《系统工程与电子技术》 EI CSCD 1999年第12期47-49,共3页
针对大气层外动能拦截器拦截弹道导弹的末制导过程 ,提出了一种新型最优制导律。由于采用了一种新的剩余时间计算方法 ,这种最优制导律产生的加速度指令可以通过拦截弹的轨控系统 (弹体纵轴方向无控 )实现。最后 ,采用新型最优制导律和... 针对大气层外动能拦截器拦截弹道导弹的末制导过程 ,提出了一种新型最优制导律。由于采用了一种新的剩余时间计算方法 ,这种最优制导律产生的加速度指令可以通过拦截弹的轨控系统 (弹体纵轴方向无控 )实现。最后 ,采用新型最优制导律和传统比例导引律分别进行了拦截过程的计算机数值仿真 ,仿真结果表明了这种新型最优制导律的有效性。 展开更多
关键词 反弹道导弹 导优制导 动能拦截器
全文增补中
Optimum Design of the Control System for a Laser Beam Riding Guidance Anti-Tank Missile 被引量:3
2
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
下载PDF
Design of Closed Loop Optimal Guidance Law Using Neural Networks 被引量:1
3
作者 ZHOU Rui 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2002年第2期98-102,共5页
It is generally impossible to obtain the analytic optimal guidance law for complex nonlinear guidance systems of homing missiles,and the open loop optimal guidance law is often obtained by numerical methods,which can ... It is generally impossible to obtain the analytic optimal guidance law for complex nonlinear guidance systems of homing missiles,and the open loop optimal guidance law is often obtained by numerical methods,which can not be used directly in practice.The neural networks are trained off line using the optimal trajectory of the missile produced by the numerical open loop optimal guidance law,and then,the converged neural networks are used on line as the feedback optimal guidance law in real time.The research shows that different selections of the neural networks inputs,such as the system state variables or the rate of LOS(line of sight),may have great effect on the performances of the guidance systems for homing missiles.The robustness for several guidance laws is investigated by simulations,and the modular neural networks architectures are used to increase the approximating and generalizing abilities in the large state space.Some useful conclusions are obtained by simulation results. 展开更多
关键词 neural networks missile guidance optimal guidance law proportional navigation guidance
下载PDF
上一页 1 下一页 到第
使用帮助 返回顶部