Then, based on the decomposition of task section plane of general missile control software, the procedures for the operational reliability .
对综合控制软件的任务剖面进行了分解，并给出了软件在系统测试与飞行试验阶段运行可靠度的计算方法。
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。
Based on adaptive backstepping control techniques and fuzzy-neural theory, a sliding mode control scheme is proposed for missile control systems with uncertainties.
阐述了在导弹系统存在不确定性情况下，基于自适应反演控制技术和模糊神经网络理论，提出了一种导弹滑模控制系统设计方法。
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。
Based on RBF neural networks and backstepping control techniques, a nonlinear adaptive controller design method is proposed for missile control systems with a general set of uncertainties.
在导弹系统存在广义不确定性情况下，提出了一种基于反演设计技术和RBF神经网络的导弹非线性自适应控制系统设计方法。
Considering the difference of the rolling missile and the non-rolling missile, the mechanism of rolling missile control force and the control theory of rolling missile was analyzed rigorously.
考虑到滚转导弹与非滚转导弹的不同，本文仔细分析了滚转导弹控制力的产生机理和滚转导弹的控制原理。
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。
He made clear he would not accept Moscow's linkage between arms control and missile defence, a statement that suggests there is little prospect of a rapid breakthrough.
他明确表示，他不能接受莫斯科把军控和导弹防御互相挂钩；这意味着，谈判能迅速取得突破的可能性很小。
Logically speaking, this control list will include equipment, material and technology that can be directly used in missiles, as well as missile-related dual use items.
从逻辑上讲，这一清单将包括直接用于导弹的设备、材料和技术，以及与导弹相关的双用途物项。
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。
So the recent introduction of the microcomputer has provided a further impetus towards the possibility of on-line optimization, or true adaptive control, within the missile itself.
最近微型计算机的出现，一定会促进联机最佳化，或者导弹内部的真正的适应控制的可能性。
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。
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。
This paper investigates the large Angle attitude post stall maneuver control for the agile turn phase of an air-to-air missile that has high off-boresight capability and head reverse maneuverability.
为研究具有大离轴角及越肩发射能力的先进空空导弹初始段敏捷转弯方法，研究了装有反作用喷气控制系统的空空导弹的大角度姿态过失速机动控制律。
This paper deals with the near-minimum-time attitude maneuver control of vertical launching tactical missile, in order to solve fast attitude maneuver of this kind of missile.
针对战术导弹垂直发射姿态调转时的快速性要求，研究了垂直发射快速姿态调转的次最小时间控制问题。
This paper integrates direct lateral force control with aerodynamic control, taking the anti-aircraft missile which has the anti-guided ability in the aerosphere as research subject.
本文的研究对象为大气层内具有反导能力的防空导弹。主要研究内容为把直接侧向力控制与气动力控制结合。
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。
This can lead to lots of frantic battles to control the various missile silos, as they periodically loft up a missile that can damage the energy shield.
这个特点会为了控制各种导弹发射井而引发众多的激烈战役，因为这些导弹发射井可以阶段性地发射导弹，击毁能量盾。
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。
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。
Firstly, the situation of excessive dynamic stress during vibration test of environmental stress screening for an air-air missile flight control cabin was introduced.
首先介绍空空导弹飞控舱环境应力筛选随机振动试验过程中出现振动过应力的情况，然后对出现振动过应力的原因进行了分析。
Aiming at the tracking control problem of missile electro-hydraulic servo mechanism, a method of fuzzy sliding mode control based on sliding mode condition is presented.
针对导弹电液伺服机构的跟踪控制问题，设计了一种基于滑模产生条件的模糊滑模控制方案。
Aiming at the tracking control problem of missile electro-hydraulic servo mechanism, a method of fuzzy sliding mode control based on sliding mode condition is presented.
针对导弹电液伺服机构的跟踪控制问题，设计了一种基于滑模产生条件的模糊滑模控制方案。
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