missile control信息详情
导弹控制
missile───adj.导弹的；可投掷的；用以发射导弹的；n.导弹；投射物
regulus missile───雷格斯导弹
fagot missile───法格特导弹
cruise missile───n.巡航导弹；n.[航][军]巡航导弹
missile defense───导弹防御
blowgun missile───喷枪导弹
deflect missile───偏转导弹
guided missile───导弹；导向飞弹；有线导引飞弹；n.导向飞弹，导弹
harpoon missile───鱼叉导弹
A design method of adaptive flight control system for certain missile control system is introduced in this paper, in which adaptive control theory can be applied.───针对某型导弹控制系统，通过自适应控制理论的应用，介绍了一种自适应制导控制系统的构建方法。
severe threat of electromagnetic pulse weapon to ballistic missile control systems, the primary ways how control system counteract HEMP are discussed.───针对电磁脉冲武器对导弹控制系统的严重威胁，重点阐述控制系统抗核电磁脉冲(HEMP)的主要途径。
To avoid the affect of sneak circuit to firing control circuit of aviation weapon, a sneak circuit analysis is performed to a certain missile control system.───为排除潜电路对航空武器发射的影响，以某型号飞机和某型号导弹发射架控制电路为例，对该型号导弹发射控制电路的潜电路进行了分析。
He began his career overseeing site purchases and construction, and eventually took a position on a missile control crew.───他的工作开始时是负责监管采购和工程建设，后来，他成为了导弹控制组的成员。
An example is given to show how the SLAM is applied to the error analysis of a tactical missile control system.───研究了统计线性化伴随方法在小型战术导弹控制系统误差分析中的具体运用方法。
The missile control system composed of two pares, the controller and the controlled object.───粗略地看，导弹控制系统都是由控制器和被控对象两大部分组成的。
The researching result in this paper possesses a value of application and theory in FDD of missile control system.───本文的研究成果对控制系统的故障诊断有应用价值和理论意义。
Several Problems Study and Adapter Design for the Hardware-in-the-Loop Simulation Platform of a Missile Control System───导弹控制系统半实物仿真研究与适配器设计
Study of Variable Structure Control for the Air-to-Air Missile Control System───变结构控制在空空导弹控制系统中的应用研究
To avoid the affect of sneak circuit to firing control circuit of aviation weapon, a sneak circuit analysis is performed to a certain missile control system.
Simulation of one missile control and guide system shows that the proposed estimating method provides a good interface condition between midcourse guidance and terminal guidance.
Simulation of one missile control and guide system shows that the proposed estimating method provides a good interface condition between medial guidance and terminal guidance.
Based on the mathematical model of air-to-air missile control system, a variable structure control law is designed.
Coupling factors of BTT missile control system is qualitatively analyzed.
The missile control system is composed of two parts: the controller and the controlled plant.
Then, based on the decomposition of task section plane of general missile control software, the procedures for the operational reliability .