In considering the mechanical ambient for missile launching under water, principle and implementation for measuring the dynamic response of missile model under water are give out.
本文考虑导弹水下发射时的力学环境条件，给出了导弹模型水下点火动响应测试试验原理与实现方法。
Practical tests of launching under water have been carried out based on a missile model, and parameters such as driving force of the engine and the structural strain of the model are obtained.
并基于某导弹缩比模型进行了实际测试，取得了导弹模型水下发射时发动机推力以及相应的结构壳体应变量等参数。
This paper introduce the mathematical model to realize the electronic analog computation to missile allowable launching distance and explain the transforming way of radar range scale.
介绍了为实现电子模拟运算导弹允许发射距离的数学模型，并说明了雷达距离比例尺的变换方法。
In the case of lacking remote signal of the missile at flying extremity, it is a credible method to recur the data of movement parameter at that time using grey forecast model.
在导弹飞行末段遥测信号缺失的情况下，采用灰色预测模型对导弹飞行末段的运动参数进行数据重现是一种较为可信的方法。
Considering some uncertain influencing factors in the missile cost estimation, this paper provides a more effective BP neural network to set up the estimation model of the missile cost.
文中提出了一种更有效的前向BP神经网络，考虑了导弹成本中的一些非确定性的影响因素，建立了导弹成本的估算模型。
A mathematical model is established solely according to two kinds of warhead fuze modes considering that atmosphere parameter error works on the flight of warhead explosion spot of ballistic missile.
以等高程和等过载引信两种弹头引信方式建立了大气参数偏差对弹道式导弹弹头引爆点射程影响的数学模型；
Based on the analysis of theory data, this paper brings the base model of wireless narrow-band channel for air-based missile image transmission system.
在理论分析的基础上，结合对大量试验数据的分析，给出了空基型导弹图像传输系统无线窄带信道的基本模型。
According to the WSEIAC model, an index hierarchy of ground antiaircraft missile armament system's efficiency has been developed, and its corresponding three BP nerve network was established.
根据WSEIAC模型建立了地面防空导弹武器系统效能评估的指标体系，并依此模型建立与之对应的三层BP神经网络。
The results from the ability of satisfactory and can be used to quantize the ability of air defense missile systems to intercept targets under the conditions given by using an ideal efficiency model.
分析得到的结果是令人满意的，从而进一步解决了如何通过较理想的效能模型，全面地预测防空导弹武器系统在给定条件下完成规定任务的能力问题。
Through the analysis to firing model of the launching control system for a certain type conventional tactical missile, the firing accuracy to the target is discussed.
本文旨在通过对某类常规战术导弹发射控制系统射击模型的分析，探讨导弹打击目标的精确度。
Through analyzing the ordering conduct of anti-ship missile, an ordering model is designed, and several order strategies are discussed in order to find a better ordering strategies combination.
文章通过对反舰导弹的订货行为分析，设计了一种订货模型，并对可能出现的几种订货策略进行讨论，以期寻求一个周期内的合理订货策略组合。
This new model can get over the limit that only evaluates the effectiveness in experimentation, and the evaluation can reflect the missile performance in real battle.
此模型突破了只能评估导弹武器系统试验效能的局限性，估算值更能反映出导弹武器系统的实战水平。
According to the analysis and derivation, the dynamic model of the Leader Missile in Launch coordinate is built.
根据运动学分析与推导，得到主弹在地面发射坐标系下的运动模型。
Aiming at the pitching movement model, a nonlinear variable structure controller with an optimal sliding surface for the pitching control system of missile was presented.
针对俯仰运动模型，提出利用非线性最优滑模控制来设计某型导弹的俯仰运动控制系统。
According to force analyzing of missile, the complicated force calculation has been replaced by the fitting formula, and a simplified trajectory model has been developed.
根据导弹受力特性分析，用拟合公式替代了复杂的外力计算，并建立了简化的外弹道模型。
Taking missile attacking large size moving target as example, the operational effectiveness model of the satellite was built with probability of hitting target as measure of effectiveness.
以支持导弹打击大型移动目标为例，以命中目标概率为作战效能指标，建立了光学成像侦察卫星作战效能模型。
The mission section, the constrain conditions, the weight composition of the maneuverable missile, and the model of used in turbofan engine maneuverable missile were presented.
简述了飞航导弹任务剖面、约束条件的给定、导弹的重量组成以及涡扇发动机模型。
Finally, calculation is made on typical long range ballistic missile according to the model. The results shows that the formulas can meet required precision in correction before the launch.
并按该计算模型，对典型远程导弹进行了计算，结果表明，该修正公式计算精度高，能用于导弹射前修正。
The analysis model of comprehensive performance of submarine launched anti ship missile based on gray correlative is established according to gray system theory.
根据灰色系统理论建立了潜射反舰导弹综合性能灰关联分析模型，以灰色关联度为基本依据构造出导弹综合性能评估指数。
On the basis of creating the index system of information operation capability of missile troop, AHP is used to distribute weight vectors, and fuzzy synthetic evaluation model is given out.
在分析、确定了导弹部队信息作战能力评估指标体系的基础上，运用AHP法分配了权重，建立了基于模糊综合评估方法的信息作战能力评估模型。
On the basis of impulse fundamentals and short offset theory, a calculation method and its model of missile hit error generated by after-working impulse are given.
根据冲量原理和小偏差理论给出了后效冲量误差引起导弹命中误差的一种计算方法和模型，提出了一种用关机分离方程控制射程的方法。
The unitary missile target kinematics model is established based on the relative kinematics firstly. Then the guidance law is designed using variable structure system theory.
首先在相对运动学的基础上建立了归一化的导弹—目标的运动学模型，然后利用变结构控制理论设计了导引律。
The fragmentation artillery warhead is utilized in the paper. The target damage tree is used to build vulnerability model by means of analyzing the vulnerability of vehicle of launching missile.
本文采用战斗部为破片式战斗部，通过对导弹发射车的易损性分析，目标毁伤树来建立目标易损性计算模型。
The mathematic model of selection based on entropy weight and matter analysis is set up according to the characteristics of position selection of some anti-aircraft missile weapons.
根据某型防空导弹阵地选择的特点，利用信息熵权重和物元分析的方法建立了阵地优选的数学模型。
Based on the method of fuzzy intersection calculation, evaluation index system and fuzzy evaluation model of command ability for commander of tactical missile are established.
运用基于模糊交集运算的分析方法，建立了战术导弹指挥员指挥能力评价指标体系及模糊评价模型。
This paper USES the method of analysing fuzzy set and set up a model of time series multiple levels fuzzy synthetic judgement. And the factors affecting the missile price are explained at quantity.
本文利用模糊集分析的方法，量化了影响导弹价值的因素，建立了关于导弹定价的时序模糊综合评判模型。
According to the demand of flight control system, a nonlinear dynamics model with considerable aerodynamic forces and moments for a large maneuver re entry missile head is built.
根据飞行控制要求，考虑了影响较大的气动力和气动力矩因素，建立了一个完全表征大机动情况下弹头运动的非线性动力学模型。
Based on the hardware structure and operation principle of the missile rudder electric loading system, the causation, mathematic model and test method of surplus torque are analyzed.
导弹舵电动加载系统的硬件结构和工作原理的基础上，因果关系，多余力矩的数学模型和测试方法进行了分析。
FAS thinks, the emissive platform here is originally vintage "east wind - 4" model strategic missile design, China upgrades it after transforming, can blast off new-style "east wind - 21" missile.
FAS认为，这里的发射平台本为老式“东风-4”型战略导弹设计，中国把它升级改造后可以发射新型“东风-21”导弹。
Based on the rotor free-wake model and the rotor trim model, an analytical method is developed for the prediction of helicopter rotor induced velocities on missile trajectory.
应用自由尾迹方法和旋翼配平模型，建立了一个悬停和前飞状态旋翼在导弹发射线上的诱导速度计算模型。
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