青年中文missile control的意思
missile control中文翻譯：
導彈控制
missile───adj.導彈的；可投擲的；用以發射導彈的；n.導彈；投射物
regulus missile───雷格斯導彈
fagot missile───法格特導彈
cruise missile───n.巡航導彈；n.[航][軍]巡航導彈
missile defense───導彈防御
blowgun missile───噴槍導彈
deflect missile───偏轉導彈
guided missile───導彈；導向飛彈；有線導引飛彈；n.導向飛彈，導彈
harpoon missile───魚叉導彈
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.───針對某型導彈控制系統，通過自適應控制理論的應用，介紹了一種自適應制導控制系統的構建方法。
severe threat of electromagnetic pulse weapon to ballistic missile control systems, the primary ways how control system counteract HEMP are discussed.───針對電磁脈沖武器對導彈控制系統的嚴重威脅，重點闡述控制系統抗核電磁脈沖(HEMP)的主要途徑。
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.───為排除潛電路對航空武器發射的影響，以某型號飛機和某型號導彈發射架控制電路為例，對該型號導彈發射控制電路的潛電路進行了分析。
He began his career overseeing site purchases and construction, and eventually took a position on a missile control crew.───他的工作開始時是負責監管采購和工程建設，后來，他成為了導彈控制組的成員。
An example is given to show how the SLAM is applied to the error analysis of a tactical missile control system.───研究了統計線性化伴隨方法在小型戰術導彈控制系統誤差分析中的具體運用方法。
The missile control system composed of two pares, the controller and the controlled object.───粗略地看，導彈控制系統都是由控制器和被控對象兩大部分組成的。
The researching result in this paper possesses a value of application and theory in FDD of missile control system.───本文的研究成果對控制系統的故障診斷有應用價值和理論意義。
Several Problems Study and Adapter Design for the Hardware-in-the-Loop Simulation Platform of a Missile Control System───導彈控制系統半實物仿真研究與適配器設計
Study of Variable Structure Control for the Air-to-Air Missile Control System───變結構控制在空空導彈控制系統中的應用研究
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 .