missile control system（意思翻译）

"DaoDan"控制"XiTong"

missile control system（相似词语短语）

1、missile───adj.DaoDan的；可投掷的；用以发射DaoDan的；n.DaoDan；投射物

2、deflect missile───偏转DaoDan

3、missile defense───DaoDan防御

4、blowgun missile───喷枪DaoDan

5、cruise missile───n.巡航DaoDan；n.[航][军]巡航DaoDan

6、regulus missile───雷格斯DaoDan

7、executive control system───[计]执行控制XiTong

8、fagot missile───法格特DaoDan

9、control system───Cao纵XiTong; 控制设备; 控制XiTong; 控制制度；[自]控制XiTong

missile control system（双语使用场景）

1、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DaoDan发射架控制电路为例，对该型号DaoDan发射控制电路的潜电路进行了分析。

2、Study of the Technology of Optical Fiber Transmission in Missile Control System───DaoDan控制XiTong的光纤传输技术研究

3、Several Problems Study and Adapter Design for the Hardware-in-the-Loop Simulation Platform of a Missile Control System───DaoDan控制XiTong半实物FangZhen研究与适配器设计

4、Study of Variable Structure Control for the Air-to-Air Missile Control System───变结构控制在空空DaoDan控制XiTong中的应用研究

5、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XiTong的故障诊断有应用价值和理论意义。

6、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DaoDan控制XiTong误差分析中的具体运用方法。

7、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DaoDan控制XiTong，通过自适应控制理论的应用，介绍了一种自适应制导控制XiTong的构建方法。

8、The missile control system composed of two pares, the controller and the controlled object.───粗略地看，DaoDan控制XiTong都是由KongZhiQi和被控对象两大部分组成的。

9、precision of gyro is one of the most important points to decide precision of missile control system and it is mostly effected by the gyro random drift.───DaoDan控制XiTong中，陀螺精度是XiTong精度的重要指标之一，而陀螺仪随机漂移是影响陀螺精度的重要误差源，因而研究陀螺仪随机漂移对提高陀螺精度有着重要意义。

missile control system（英语使用场景）

1、Based on the mathematical model of air-to-air missile control system, a variable structure control law is designed.

2、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.

3、The missile control system is composed of two parts: the controller and the controlled plant.

4、Coupling factors of BTT missile control system is qualitatively analyzed.

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