Miss missile

与Miss missile相关的网络例句 [注：此内容来源于网络，仅供参考]

Aircraft-type missile,aircraft-like missile, aircraft-shaped missile, air-supported missile, aerodynamic missile, cruise missile, pilotless missile, wing-borne missile, winged missile.

c &飞航导弹由英文& cruise missile &而来，是指在飞行过程中与地面保持一定高度、以巡航速度飞行的有翼式导弹，有时也称为巡航导弹。按照国内的分类习惯，巡航导弹中收入的是射程大于500 km的远程飞航导弹&。

To overcome the bad effect resulting from the nonlinearity time-variability and uncertainty on autopilot system performance during the motion process of aerodynamics missile, and to further improve the flight quality of missile, the autopilot system and used control method are researched. Firstly the integrant structure of system is discussed; then baaed un introducing the traditional PID method, controllers for missile attitude motion are designed respectively using fuzzy self-turning PID method and neural network self-adaptive PID method; at last a simulation experiment is finished. By comparing the simulation results that the designed controllers have good qualities is showed, and the feasibility and validity of applying fuzzy control and neural network into automatic control of aerodynamics missile is confirmed, and the base that other nonlinear control theory can be combined with the traditional control for missile to further improve the performance of missile control system is established.

为了克服飞航导弹运动过程中的非线性、时变性和不确定性对自动驾驶仪系统性能的不良影响，进一步提高导弹的飞行质量，对自动驾驶仪系统及其采用的控制方案进行了研究；首先对系统的整体结构进行了分析，然后在介绍经典PID方案的基础上，分别采用模糊自调整PID方案和神经网络自适应PID方案设计了导弹姿态运动控制器，最后进行了仿真实验；仿真结果的对比展示了所设计控制器良好的品质，验证了将模糊控制和神经网络应用于飞航导弹自动控制中的可行性和有效性，为其它非线性控制理论与导弹传统控制相结合以进一步提高导弹控制系统的性能奠定了基础。

To develop Linear Fractional Transformation model based on quasi-linear model for ground-to-air missile, state transformation method was used to establish quasi-Linear Parameter Varying model for missile longitudinal short-period dynamics by changing missile states along with an equilibrium trajectory decided by time-varying parameters. Based on the obtained quasi-LPV model, the LFT model of the missile was developed by use of MATLAB functions, and the missile dynamics were explicitly separated into certainty part and time-varying parameter part.

为了建立基于准线性化模型的地空导弹线性分式变换模型，采用状态替换方法将导弹的状态沿着一条由时变参数决定的平衡点轨迹进行变换，建立了纵向短周期动力学的准线性参数时变模型；基于所建立的准LPV模型，采用MATLAB函数建立了导弹的LFT模型，将导弹动力学明确描述为确定性部分和时变参数部分。

与Miss missile相关的网络解释 [注：此内容来源于网络，仅供参考]

MISS Missile Intercept Simulation System：导弹拦截模拟系统

MISRC Management Information System Research Center 管理信息... | MISS Missile Intercept Simulation System 导弹拦截模拟系统 | MISSIL Management Information System Symbolic Interpretive Language 管理信息...

The dismissed Swiss miss kissed the once missing missile and scissors：被解雇的瑞士小妞吻了一度失踪的导弹和剪刀

597. The cosmic verse on the reverse of the pa... | 598. The dismissed Swiss miss kissed the once missing missile and scissors. 被解雇的瑞士小妞吻了一度失踪的导弹和剪刀. | 599. The comb is combined wi...