To reduce the wind disturbance error, the wind disturbance regular pattern is studied using a missile simulation system based on the SIMULINK.
为了减小再入段风干扰造成的误差，利用在Simulink中建立的数字打靶平台对它进行了研究。
It is an important half hardware-in-loop simulation equipment, which is often used to simulate the aerodynamic torque load on the missile rudder or elevon actuators in the flight.
它是地面半实物仿真系统中的一种重要专用设备，用来模拟飞行器舵机在飞行过程中所承受空气动力力矩载荷。
The composition of the simulation system, data processing flowchart and simulation mode that included the missile dynamics, sensitive element and variable structure controller were given.
给出了该仿真系统的组成、信号处理流程，以及包括弹体动力学、敏感元件和变结构控制器的仿真模型。
The method is concise and practical, and uses advanced "fast simulation method" to calculate missile launch boundary which makes calculating velocity much faster.
该方法简洁实用，而且使用先进的快速模拟法计算导弹允许攻击区，使计算速度大大提高。
A method of constructing certain missile virtual maintenance training system was proposed based on virtual reality technology, virtual prototype technology and process simulation technology.
提出基于虚拟现实技术、虚拟样机技术和过程仿真技术的大型复杂装备虚拟维修训练系统设计方法。
Making use of computational fluid dynamics method and dynamic simulation, the thesis studies the effects of jet flow on launch process of vehicular container-type missile.
结合流场计算和发射动力学仿真，研究某型车载发射系统中燃气流对发射过程的影响。
The test for compensating of the sight line error for missile radome has been done by the semi-real simulation system, which shows the highly precise compensation for missile homing.
利用射频仿真系统对该补偿系统进行动态实物联试，试验表明该补偿系统达到了很高的补偿精度。
The architecture design of the simulation system was discussed in detail, and the modeling of target movement, interference missile and complex background scene was investigated.
讨论仿真系统的结构，目标运动、干扰弹投放和复杂背景的建模。
To investigate the rolling control characteristics of canard-controlled missile with fixed-tail, a numerical simulation method based on N-S formulation was conducted.
采用以N-S方程为主控方程的数值模拟方法，进行固定尾翼鸭式气动布局导弹的气动特性和流场数值模拟。
Due to mission profile , launched conditions and trajectory , maneuver chains for stand off missile are designed . instruction control model and maneuver model is setup for ucav flight simulation.
结合作战任务剖面、导弹发射条件和弹道，设计出无人机防区外攻击导弹发射前、后的机动动作链。
The simulation example given in this paper is devoted to the fuzzy control of missile lateral movement with the intention of exploring the possible application of fuzzy control to aeronautics.
本文给出的例子是对某型导弹横侧向运动的模糊控制，意在探索模糊控制在航空中应用的可能性。
This project is not only an improvement to the architecture but also an expansion of system's function, which means a lot to the missile flight simulation and the final navigation system.
该项目的完成不仅使惯性元件测评系统在结构设计上有了较大改进，在功能上也使其更加完备，向着最终的弹体飞行仿真及导航系统的实现迈出了一大步。
Numerical 3d simulation and research on inner nozzle and outlet flow field of solid rocket motor of long range missile designed by Russia using STAR-CD computational fluid software.
采用STAR - CD计算流体软件对某俄式发动机的喷管内流场及喷管出口处流场进行了三维的数值仿真与研究。
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.
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。
In order to reappear the fuze movement rule through testing the parameter of movement under simulation trajectory environment, the missile-borne memory test system is designed in the thesis.
为了通过测试引信在模拟弹道环境下的运动参数，再现其运动规律，本文研制了新型弹载存储测试系统。
The simulation shows the influence to the missile survivability of each parameter, proved the practicability, validity of the power series and AHP used in the study of missile survivability.
为研究先进战斗机的作战效能，通过建立对空对地统一的效能指标体系，综合采用幂指数法和模糊层次分析法对其作战效能进行评估。
The simulation results show that the implementation of missile fuzzy control algorithm on FPGA is feasible and the demand for real-time is met.
然而算法的复杂程度以及在工程上实现的可行性需要通过硬件实现效果来验证。
To study the offense-defense confrontation process of joint stand-off missile weapon systems, the computing simulation method is used.
本文从这四个阶段给出了对抗过程中武器系统生存能力的动态描述，并分析了各个阶段的计算模型。
To study the offense-defense confrontation process of joint stand-off missile weapon systems, the computing simulation method is used.
本文从这四个阶段给出了对抗过程中武器系统生存能力的动态描述，并分析了各个阶段的计算模型。
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