1) Optimal guidance
最优制导
1.
The optimal guidance law of each plane is designed,respectively,considering the minimum energy consuming and ter- minal angular constraint.
分别设计了两个平面内的最优制导律。
2.
In this paper,an improved optimal guidance law design method was proposed.
提出了一种改进的最优制导律设计方法 ,得到了可以保证末端速度方向的制导律 ,速度大小控制通常靠理想速度曲线来保证 ,按一定的规则将最优制导律与理想速度曲线结合起来就得到了满足全部要求的制导律。
3.
A strapdown combined terminal guidance system for the medium - range missile is studied and an optimal guidance command is designed.
基于最优控制理论的二次型性能指标，将弹体-自动驾驶仪惯性设计为三阶受控对象，导出了最优制导指令的解析表达式。
2) Optimal guidance law
最优制导律
1.
Based on analyzing the missile and target motion dynamics, the fuzzy rules are established according to design expert experience of optimal guidance law and characteristics of measurement noise disturbances.
进行模糊末制导律设计时,在分析导弹和来袭目标运动特性的基础上,根据最优制导律设计专家经验和测量噪声的干扰特性建立模糊规则。
2.
By using the steepest ascent method,the optimal guidance law is gained to solve this kind of problem: the final time is undefined and there are constrains.
对三种不同的拦截情况 ,进行了仿真 ,结果证明梯度投影法数值求解导弹最优制导律是可行
3) optimal middle guidance
最优中制导
1.
In this paper,an optimal middle guidance law is pointed out.
文中提出一种最优中制导律,给出了数学公式及其最优系数的具体算法,并通过仿真,验证了该制导律的有效性。
4) Optimal switching guidance
最优开关制导
5) optimal sliding-mode guidance law
最优滑模制导律
1.
An optimal sliding-mode guidance law which is robust to parameter perturbations and external disturbance is proposed for the space interception problem of maneuvering target,and an intelligent method of the guidance law is studied.
针对机动目标的空间拦截问题,文中介绍了一种对参数摄动和外干扰具有鲁棒性的最优滑模制导律,并对其智能化实现方法进行了研究。
6) optimal proportional guidance law
最优比例制导
补充资料：波束制导(见遥控制导)
波束制导(见遥控制导)
beam-rider guidance
boshu zhidao波束制导(beam一rider guidanee)见遥控制导。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条