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   missile a 的翻译结果: 查询用时:0.217秒
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missile a
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  “missile a”译为未确定词的双语例句
     In accordance with the characteristics of image sequence obtained by the imaging seeker of air-to-air missile,a passive ranging algorithm based on infrared image sequence is proposed.
     根据红外成像导引头截取时序红外图像的特点,提出了一种跟踪红外运动图像序列中目标的稳定特征点,利用成像所得特征部分尺寸得到距离信息的被动测距方法。
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     Considering constrains of the whole flight trajectory of the ballistic missile,a mathematical model of maximum range optimization was built,a corresponding simulation model was also built under the MATLAB/SIMULINK environment.
     针对弹道式导弹整个飞行弹道的多种约束要求,建立了弹道最大射程优化的数学模型,在MATLAB/SIMULINK环境中,建立相应的仿真模型。
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     According to the features related to the vertical launching tactical missile, a nonlinear dynamics model was established based on error quaternion.
     首先基于误差四元数并结合垂直发射的具体特点,建立了战术导弹垂直发射的非线性数学模型;
短句来源
     According to the features related to the vertical launching tactical missile,a nonlinear dynamics model was established based on error quaternion.
     首先基于误差四元数并结合垂直发射的具体特点 ,建立了战术导弹垂直发射的非线性数学模型 ;
短句来源
     According to the features related to the vertical launching tactical missile, a nonlinear dynamics model is established based on error quaternion.
     首先基于误差四元数并结合垂直发射的具体特点,建立了战术导弹垂直发射的非线性数学模型;
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  相似匹配句对
     Missile Propulsion
     导弹的推进技术
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     “Spreading missile technology
     导弹技术在世界的扩散
短句来源
     U.S. and Missile Controlling System
     美国与导弹技术控制体制
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     Soviet Scud Missile
     苏联的飞毛腿导弹
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查询“missile a”译词为用户自定义的双语例句

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A calculation model on the ignition parameters of the second stage rocket motor of a surface to air missile in plateau environment is presented. A calculation on the missile A and its improved version B based on the model is carried out. Through the missile target practice test in plateau environment, the cal culated results and the model are proved to be correct. The method is available to study the ignition parameters of other missile.

建立了高原条件下地空导弹二级发动机点火参数的计算模型。对地空导弹 A型及其改进后的 B型两种导弹进行了计算 ,并通过了部队高原条件下的实弹打靶试验。试验的圆满成功证明 ,该方法对研究其它地空导弹高原条件下二级发动机点火性能具有参考价值

Aiming to the problems of nonlinear time-varying and modeling error owing to fan-shaped launching and large-space maneuver for aerodynamic missile,an intelligent automatic pilot based single neuron for the flight control of missiles was studied through the theory of intelligent control,neural networks and traditional PID control in this paper.The simulation showed that the automatic pilot would provide the aerodynamic missile a good flying quality,an excellent precision and a greater robustness.Moreover,the...

Aiming to the problems of nonlinear time-varying and modeling error owing to fan-shaped launching and large-space maneuver for aerodynamic missile,an intelligent automatic pilot based single neuron for the flight control of missiles was studied through the theory of intelligent control,neural networks and traditional PID control in this paper.The simulation showed that the automatic pilot would provide the aerodynamic missile a good flying quality,an excellent precision and a greater robustness.Moreover,the controller could meet the requirement for real time,and be implemented easily.

针对飞航导弹扇面发射和大空域机动飞行引起的非线性时变、建模误差等问题,根据智能控制、神经网络及传统的PID控制理论设计了一种基于单神经元的智能自整定PID控制器。仿真结果表明,该控制器可使飞航导弹的自动驾驶仪具有较好的飞行品质和精度、更强的鲁棒性,同时也能满足实时性要求,且工程实现简单。

Applying theory of fuzzy evaluation and multi-objects optimization, this paper researches the rational disposal of missiles, about how many missiles a formation ships should carry. Adopting relevancy analysis of grey system theory, it obtains the relevancy of ideal ratio of any type of missiles, and constructs the subordinated function of attacking and defending capabilities. Solving the model of multi-objects optimization, the rational disposal for each type of missile is determined....

Applying theory of fuzzy evaluation and multi-objects optimization, this paper researches the rational disposal of missiles, about how many missiles a formation ships should carry. Adopting relevancy analysis of grey system theory, it obtains the relevancy of ideal ratio of any type of missiles, and constructs the subordinated function of attacking and defending capabilities. Solving the model of multi-objects optimization, the rational disposal for each type of missile is determined. By this algorithm, commanders can be helped to make optimal decision when the warships facing different combat missions: attacking or defending.

运用模糊理论和多目标优化理论探索舰艇编队所携带导弹的合理配置。采用灰色系统理论的关联度分析方法,得出各型导弹对理想导弹的关联度,构建进攻能力和防御能力的隶属度函数;通过多目标优化模型的求解,实现各型号导弹的最优配置。使用该优化算法,当舰艇编队面对不同的攻防任务时,能有效地辅助军事指挥员做出最优决策。

 
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