1) LQG optimal guidance law
LQG最优制导规律
1.
Based on Linear Quadratic Gaussian(LQG) theory,a LQG optimal guidance law with time-variable effective navigation ratio is studied.
研究了基于线性二次型高斯(LQG)的中远程空空导弹最优制导规律,给出了有效导航比可变的LQG最优制导规律的简化形式,对有效导航比和比例系数进行了适当简化。
2) LQG optimal control
LQG最优控制
1.
For multiple inputs and multiple outputs networked control systems(NCSs)with limited communication channels,the effects of system resource constraints on the performance of LQG optimal control is studied.
针对一类通信信道受限的多输入多输出网络控制系统(NCSs),研究有限通信系统资源对LQG最优控制性能的影响。
3) LQG optimal controller
LQG最优控制器
4) 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
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) Optimum Intermediate Guidance Law
最优中制导律
1.
The Optimum Intermediate Guidance Law of Long Distance Air-to-Air Missile;
远距空空导弹最优中制导律研究
补充资料：[3-(aminosulfonyl)-4-chloro-N-(2.3-dihydro-2-methyl-1H-indol-1-yl)benzamide]
分子式：C16H16ClN3O3S
分子量：365.5
CAS号：26807-65-8
性质：暂无
制备方法：暂无
用途：用于轻、中度原发性高血压。
分子量：365.5
CAS号：26807-65-8
性质：暂无
制备方法：暂无
用途：用于轻、中度原发性高血压。
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