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。
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.
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。
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.
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。
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.
已经发表的自寻的非滚转导弹拦截问题的数学模型往往是平面模型或空间质点模型。
Presents a space motion model (SMM) of multiple rigid bodies with varying mass for the description of the intercept problem of homing missiles with roll stabilization.
阐述了导弹武器系统作战效能的概念、量度准则、评定方法和步骤，并推导了常见的两种效能评估模型。
The concepts, measure standards, evaluation methods and steps of missile weapon system are expounded, and two effectiveness evaluation models are established.
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。
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.
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。
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.
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 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.
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。
According to force analyzing of missile, the complicated force calculation has been replaced by the fitting formula, and a simplified trajectory model has been developed.
在分析了本方案优点的基础上，建立了质量矩控制导弹的动力学模型，包括质心动力学和绕质心的动力学方程。
On basis of analyzing the advantages of the scheme, a dynamics model of MMTC was constructed, which includes centroid dynamics and dynamics moment equations of centroid.
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 unitary missile target kinematics model is established based on the relative kinematics firstly. Then the guidance law is designed using variable structure system theory.
便携式地空导弹野外训练系统模型由中央控制计算机、信号转接器、瞄准训练弹和对空指挥镜组成。
The portable anti-aircraft missile field training system consists of center control computer, signal commutator, collimated training missile and anti-air commanding lens.
文中提出的多头分导弹头模型具有较好的参考价值，对所需关键控制技术的分析设计，为深入研究提供了必要的基础。
According to the provided plan of MITRV, this article designed the model of MITRV with current technologies; meanwhile, it analyzed and designed control system in the plan.
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。
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.
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；
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.
考虑了对机动导弹实施机动区域打击，建立起在圆环形区域瞄准点选取模型，并通过计算机模拟进行了结果分析。
Attacking the mobile missile base is considered and an aim-point-choosing model for striking its ring mobile region is presented. The simulation model is realized and the result is analyzed.
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 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.
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。
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.
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。
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.
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 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.
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。
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.
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。
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.
同时利用等效密度有效地简化模型，为导弹大型有限元模型的模态估计提供了一种简单可行的方法。
Making use of equivalent density the model is simplified effectively, a simple and feasible method is offered for mode estimation of a missile's large-scale finite-element model.
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。
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.
本文在对拦截决策过程进行分析的基础上，给出了采用0—1整数规划的地空导弹武器拦截方案的优化决策模型，以使防空作战决策更加科学、实用。
Based on the 0-1 integer programming, the optimizing decision model is proposed in this paper. It can guarantee the rationality and utility of intercepting decision.
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。
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.
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。
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.
根据作战效果指标，建立了单发反舰导弹突防概率模型，研究了反舰导弹双发齐射的效果并论证了其合理性。
Base on the operational effect indexes, the penetration probability model of a single ASM is established. And then the effect and rationality of double-missiles fusillading are analyzed.
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。
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.
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。
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.
应用推荐