The precision of gyro is one of the most important points to decide precision of missile control system and it is mostly effected by the gyro random drift.
导弹控制系统中，陀螺精度是系统精度的重要指标之一，而陀螺仪随机漂移是影响陀螺精度的重要误差源，因而研究陀螺仪随机漂移对提高陀螺精度有着重要意义。
To avoid the affect of sneak circuit to firing control circuit of aviation weapon, a sneak circuit analysis is performed to a certain missile control system.
为排除潜电路对航空武器发射的影响，以某型号飞机和某型号导弹发射架控制电路为例，对该型号导弹发射控制电路的潜电路进行了分析。
With the severe threat of electromagnetic pulse weapon to ballistic missile control systems, the primary ways how control system counteract HEMP are discussed.
针对电磁脉冲武器对导弹控制系统的严重威胁，重点阐述控制系统抗核电磁脉冲(HEMP)的主要途径。
A design method of adaptive flight control system for certain missile control system is introduced in this paper, in which adaptive control theory can be applied.
针对某型导弹控制系统，通过自适应控制理论的应用，介绍了一种自适应制导控制系统的构建方法。
Optical fiber technology is used in missile control system, which can resolve the electromagnetic interfere, the electric isolation, anti-jamming and so on in control system effectively.
光纤技术用于导弹控制系统中，有效解决了控制系统的电磁兼容、电气隔离、抗干扰等问题，大大提高了导弹控制系统的性能与可靠性。
In this paper, a nonlinear adaptive control scheme for missile control system with mismatched uncertainties is proposed on the basis of RBF neural networks and inverse control technology.
在导弹系统存在非匹配不确定性的情况下，提出了一种基于RBF神经网络和反演控制技术的神经网络自适应导弹控制系统的设计方法。
Moscow however wanted control over the eastern sector of Nato's missile defence systems and a written pledge that the system will never be used against Russia.
然而，莫斯科希望能控制东边区域的北约导弹防御系统，并且能得到书面保证，该系统永远不用来对付俄罗斯。
Lockheed Martin successfully conducted a test of the new upgraded guidance and control system for the Army Tactical Missile system (ATACMS) at White Sands Missile Range.
在白沙导弹试验场，洛克西德马丁公司对陆军战术导弹系统(ATACMS)新升级的导航和控制系统进行了一次成功的测试。
It incorporates active radar with an inertial reference unit and micro-computer system, which makes the missile less dependent upon the fire-control system of the aircraft.
它把主动雷达和一个被动参考单元以及微电脑系统结合在一起，可使得导弹更少的依靠飞机上的发射控制系统。
NLOS-LS takes targeting information from the command and control center and sends it to the NLOS-LS CLU's computer and communications system for initial missile targeting.
NLOS - LS从指挥控制中心获取初始导弹目标信息，并传送到NLOS - LSCLU的计算机和通信系统。
According to a predetermined trajectory, ballistic missile with rocket engine propulsion takes a flight to intended targets under the action of the control system.
弹道导弹是用火箭发动机推进，在控制系统作用下按预定的弹道飞行至预定攻击的目标。
The design and development methods of aeroengine anti-surge control system are presented. Effects of heat disturbance parameters on the engine are analyzed during missile launch.
提出了航空发动机防喘控制系统设计和研制方法，分析了当战斗机发射导弹时热扰动参数对发动机的影响。
The method for consistency check of multisensor data by using the probability distance measuring is presented, and it used in CAN bus missile guidance and control system based on multi-IMU.
提出了应用概率距离测量对多传感器信息进行一致性检验的方法，并将此方法引入到基于多惯性测量组合的总线式导弹制导控制系统中。
A very severe nonlinear is presented because flight parameters vary along with the flight condition in the flight of missile which brings much difficulty to the design of control system.
导弹在飞行过程中，其飞行参数随着飞行条件的变化而发生较大变化，呈现严重的非线性，给控制系统的设计带来较大困难。
The key problem is that the decoupling method and the harmonious control should be studied in the missile flight simulator system control.
所以，在大系统控制中，首要问题是研究解耦方法和协调控制。
This method are with a high accuracy and real time application, and can be applied in the calculation of allowable launching area of air to air missile in air borne fire control system.
提出了一种确定目标进入角的原理和方法，这种原理和方法具有较高的计算精度和实时性，易于工程实现，可用于机载火力控制系统完成空对空导弹允许发射区计算。
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。
As a synthesis method in control system, the sliding mode of variable structure control is invariable, and which is its most excellent advantage in the missile attitude control system.
变结构控制作为控制系统的一种综合方法，它的滑动模态具有不变性，这是变结构控制在导弹姿态控制中最突出的优点。
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。
The portable anti-aircraft missile field training system consists of center control computer, signal commutator, collimated training missile and anti-air commanding lens.
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。
A low cost missile ground test and control system adopts distributed structure, which can carry out launch control, time sequence detection and pyrotechnics channel resistance measurement.
导弹地面测发控系统可以对导弹进行发射控制、时序检测和火工品通路阻值测量，其整体构成采用分布式结构。
In fact, after the America national missile defense system is deployed on a global scale, the United States can control all other country, of courses, including its friends and Allies.
事实上，美国国家导弹防御系统一旦在全球部署，可使美国能控制世界上所有国家，当然也包括其朋友和盟国。
This paper deeply studies these problems. Several methods of the control of systems with nonsmooth nonlinearities are presented and applied to air-ground missile system.
本文就此类问题展开深入研究，提出几种能克服不光滑非线性影响的控制系统设计方法，并将所提出的控制方法应用到空地导弹控制系统中。
The antiaircraft missile′s command and control system is a distributed real-time multitask data processing system, its feature is real-time, parallel processing, asynchronous and multitask.
防空导弹武器指控系统是一个分布式实时多任务数据处理系统，其特点是实时性、并发、异步和多任务。
These conclusions can be used for system design of rotating missile in the attitude control system and selection of structure and pneumatic parameters for supersonic fluidic elements.
所得结论可为旋转弹姿态控制系统的总体设计以及超音速射流元件的结构及气动参数选择提供依据。
In order to enter into the ideal trajectory with minimal energy, the nonlinear thrust vector control and the prediction guidance are adopted in the missile guidance control system.
为使飞行器能在主动段很快地进入到理想弹道上，系统采用了非线性的推力向量控制及预测制导方法。
Aiming at a guided missile, the controller is introduced on the basis of the classical control system. An autopilot for a kind of missile is designed by the theory of Fuzzy-PID control.
针对某型导弹，本文采用在传统控制系统的基础上引入模糊pid控制器的方法，应用模糊pid控制理论设计了一种导弹自动驾驶仪。
Actuality research station in-out country and production of our team in guidance of missile and control system are discussed. At last, application foreground of this investigation is explained.
总结了国内外在人眼视觉系统方面的研究现状及本课题组对于仿生技术在导弹制导、控制系统中的应用研究的主要内容、已取得的成果以及研究成果的应用前景。
Applied method and measurement accuracy of difference GPS technology on missile fire control system and its development prospect are introduced based on applied practice.
结合应用实践，论述了差分gps在导弹火控系统精度试验中的应用方法、测量精度及其发展前景。
Applied method and measurement accuracy of difference GPS technology on missile fire control system and its development prospect are introduced based on applied practice.
结合应用实践，论述了差分gps在导弹火控系统精度试验中的应用方法、测量精度及其发展前景。
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