mlrs

New Method for Simulating the Precision of Fire of MLRS

多管火箭射击精度仿真试验新方法

Combining the simple control and ballistic theory , the simulation system of precision of fire of MLRS is established .

结合简易控制和弹道理论，建立多管火箭射击精度仿真系统。

Simulation Analysis System for MLRS Initial Disturbance Based on Virtual Prototype

基于虚拟样机的多管火箭起始扰动仿真系统

Study of Shot Accuracy Reduced Computation Method for Long Range MLRS

远程多管火箭射击精度折合方法研究

Sliding Mode Variable Structure Control Strategy of AC Position Servo System of MLRS

火箭炮交流位置伺服系统滑模变结构控制策略

The test results show that firing dispersion of MLRS is improved .

试验结果表明该新技术大幅度提高了某多管火箭射击密集度。

Analysis of Ballistic Characteristics for Target Sensitive Projectile of MLRS

多管火箭末敏弹系统弹道特性分析

The new technology is developed by optimizing firing order and firing interval of MLRS .

对某多管火箭，通过优化射击顺序和射击时间间隔，形成了提高多管火箭射击密集度新技术。

Study of Diffusion in Technology Innovation Based on Agent Simulation of Random Launch and Flight Dynamics of MLRS

基于多代理的科技创新传播模型与仿真多管火箭随机发射与飞行动力学仿真

Influence of Firing Interval on Dynamics Characteristic of MLRS

射击间隔对多管火箭动态特性的影响

Simulation of Random Launch and Flight Dynamics of MLRS

多管火箭随机发射与飞行动力学仿真

Simulation and the Bayes Method Appraised the Firing Accuracy of Long-Range MLRS

仿真与Bayes方法鉴定远程多管火箭炮射击精度

Influence of Firing Orders on Performance of MLRS

射序对多管火箭武器性能影响

The simulation results show that the firing dispersion corresponding to different firing intervals of MLRS is different .

仿真结果表明多管火箭不同射击间隔下的密集度不同。

The vibration characteristics and dispersion corresponding to different firing orders of MLRS were numerically simulated .

对某多管火箭武器不同射击顺序下对应的振动特性和密集度进行数值仿真。

The simulated results of vibration characteristics , response of MLRS in launching process were verified by series of tests .

对远程多管火箭在发射过程中振动特性和动力响应进行了数值仿真，仿真结果得到了试验结果的验证。

A new method acquired from the simulation system has reduced the number of rockets used in dispersion test for one MLRS by 82.5 % .

由仿真系统仿真得出的某多管火箭武器密集度试验方案减少了试验用弹量82.5%。

The analysis on dynamics of multiple launch rocket system ( MLRS ) are the premise and key for evaluating and improving the performance of MLRS .

多管火箭动力学分析是评估和提高多管火箭性能的前提和关键。

According to the theory of the launching random dynamic of MLRS , the virtual prototype software was re-designed for the random simulation model of MLRS .

依据多管火箭发射随机动力学的理论分析，运用虚拟样机软件的二次开发功能，建立了多管火箭发射系统随机仿真模型。

Tubes firing dispersion test scheme for a 40 tubes MLRS was presented using this simulation system . Using the new scheme , rocket consumption is decreased by 82 5 % .

针对某40管火箭炮武器系统，获得了7发连射的密集度试验方案，使试验用弹量比常规试验方法减少了82.5%。

Know the different types of artillery and how to employ them effectively . Mortars , howitzers , and MLRS systems all have distinct characteristics and uses .

了解各种火炮的性能并有效利用。迫击炮，榴弹炮和多管火箭发射系统都有着截然不同的性能和效用。

So the study makes an easy way for launching research of MLRS and prepares for applying some mathematics methods ( such as CADET ) in the statistic field of MLRS .

也为采用某些数学方法（如协方差描述函数法）进一步研究火箭发射系统的统计性能作了必备的前提工作。

More than two controllable resistance states were obtained by applying DC bias sweep and voltage pulses . The resistance switching behavior shows obvious multilevel resistance switching ( MLRS ) . 2 .

采用直流偏压和脉冲电压的激励均可获得两个以上的稳定的电阻态，表明此电阻开关效应具有多级电阻开关特性。

The grey GM forecasting model for the cost estimate of MLRS is built based on reality of rare samples , while grey accumulated error model is exemplified that it can not always improve the forecasting precision .

估算了各方案的研制费用。建立了研制费用估算的灰色GM预测模型，例证了灰色累加残差模型并不一定总能提高GM模型的预测精度；

The influence of firing order and firing interval on vibration characteristic and firing dispersion of multiple launch rocket system ( MLRS ) was analyzed . The method to improve firing dispersion by optimizing firing order and firing interval was presented .

研究多管火箭射击顺序和射击时间间隔对其振动特性和密集度等系统性能的影响，为优化射击顺序提高射击密集度提供直接的方法。

By applying it into the evaluation of certain MLRS weapons system improvement scheme , the models or methods in original decision support software are improved , and the intelligent decision of weapons system schemes based on its domain knowledge is resolved by this software .

将其用于某火箭武器系统改进方案的评价中，改进原有评价软件中的模型方法，实现了借助领域知识库的武器系统方案评价的智能决策。

The lymphocytes from the healthy volunteer ( stimulating cells ) were used to stimulate the lymphocytes from the SLE patients ( reacting cells ) and the two lymphocytes were cultured together as bidirectional mixed lymphocyte reactions ( MLRs ) .

SLE患者外周血淋巴细胞作为反应细胞，健康志愿者外周血淋巴细胞作为刺激细胞，进行双向混合淋巴细胞培养（MLRs）。

Finally , computer simulating results of two kinds of sliding mode variable structure control are given . The results showed that this control strategy has stronger robustness and parameter stability , and it can be suitable for load disturbing moment and transformation of moment of inertia of MLRS .

最后给出了两种滑模变结构控制结构的计算机仿真结果，结果表明该控制策略具有较强的抗负载扰动能力和参数鲁棒性，可以适应多管火箭炮的负载干扰力矩以及转动惯量的变化。

By studying the theory of launch and flight dynamics of Multiple Launch Rocket System ( MLRS ) from the point of whole system including launching device , rockets , propellant and environment , the simulation system of random launch and flight dynamics of MLRS is established .

该文从武器全系统弹、炮、药、环境一体化的角度，在多管火箭发射与飞行动力学的理论研究的基础上，形成了多管火箭随机发射与飞行动力学数值仿真系统。