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guided missile相关的网络例句

查询词典 guided missile

与 guided missile 相关的网络例句 [注:此内容来源于网络,仅供参考]

Aircraft-type missile,aircraft-like missile, aircraft-shaped missile, air-supported missile, aerodynamic missile, cruise missile, pilotless missile, wing-borne missile, winged missile.

c &飞航导弹由英文& cruise missile &而来,是指在飞行过程中与地面保持一定高度、以巡航速度飞行的有翼式导弹,有时也称为巡航导弹。按照国内的分类习惯,巡航导弹中收入的是射程大于500 km的远程飞航导弹&。

For air interdiction missions, the aircraft could carry Kh-29T (AS-14A Kedge) TV-guided air-to-surface missile, Kh-59 (AS-13 Kingbolt) command guided ASM, Kh-59ME (AS-18 Kazoo) TV-guided air-to-surface missile, and KAB-500Kr or KAB-1500Kr TV-guided bombs.

执行空中封锁任务时,可携带Kh-29T 电视制导空对地飞弹、Kh-59 指令制导飞弹、Kh-59ME 电视制导飞弹,以及KAB-500Kr 或 KAB-1500Kr 电视制导炸弹。

To overcome the bad effect resulting from the nonlinearity time-variability and uncertainty on autopilot system performance during the motion process of aerodynamics missile, and to further improve the flight quality of missile, the autopilot system and used control method are researched. Firstly the integrant structure of system is discussed; then baaed un introducing the traditional PID method, controllers for missile attitude motion are designed respectively using fuzzy self-turning PID method and neural network self-adaptive PID method; at last a simulation experiment is finished. By comparing the simulation results that the designed controllers have good qualities is showed, and the feasibility and validity of applying fuzzy control and neural network into automatic control of aerodynamics missile is confirmed, and the base that other nonlinear control theory can be combined with the traditional control for missile to further improve the performance of missile control system is established.

为了克服飞航导弹运动过程中的非线性、时变性和不确定性对自动驾驶仪系统性能的不良影响,进一步提高导弹的飞行质量,对自动驾驶仪系统及其采用的控制方案进行了研究;首先对系统的整体结构进行了分析,然后在介绍经典PID方案的基础上,分别采用模糊自调整PID方案和神经网络自适应PID方案设计了导弹姿态运动控制器,最后进行了仿真实验;仿真结果的对比展示了所设计控制器良好的品质,验证了将模糊控制和神经网络应用于飞航导弹自动控制中的可行性和有效性,为其它非线性控制理论与导弹传统控制相结合以进一步提高导弹控制系统的性能奠定了基础。

To develop Linear Fractional Transformation model based on quasi-linear model for ground-to-air missile, state transformation method was used to establish quasi-Linear Parameter Varying model for missile longitudinal short-period dynamics by changing missile states along with an equilibrium trajectory decided by time-varying parameters. Based on the obtained quasi-LPV model, the LFT model of the missile was developed by use of MATLAB functions, and the missile dynamics were explicitly separated into certainty part and time-varying parameter part.

为了建立基于准线性化模型的地空导弹线性分式变换模型,采用状态替换方法将导弹的状态沿着一条由时变参数决定的平衡点轨迹进行变换,建立了纵向短周期动力学的准线性参数时变模型;基于所建立的准LPV模型,采用MATLAB函数建立了导弹的LFT模型,将导弹动力学明确描述为确定性部分和时变参数部分。

The dynamics model of missile sealifts system for navy ships connected parallely is established. The dynamics simulation analysis of system is studied. The dynamics characteristic of missile box on the condition of different sea states and place parameters of crane are analyzed. The theory and technology bases for the design of system of missile sealifts or navy ships connected parallely are presented. The controlled multibody system dynamics of the system of missile sealifts with wave compensation for navy ships connected parallely is presented. On the condition of stochastic momevement of depot ship and incept ship and under the action of sealifts and wave compensation, the dynamics of sealifts system is studied by using discrete time transfer matrix method of multibody system. The calculate method of electric machine impule is developed in the process of supplying missile and action of wave compensate. Based on the PLC control system, the control method, which control supply process by testing torque of guide strings is presented.

本文建立了舰艇并靠导弹补给动力学模,进行了舰艇并靠导弹补给及波浪补偿系统动力学仿真分析,获得了导弹箱在不同海况下和舰用起重机不同位置参数的运动规律,为舰艇并靠导弹补给系统设计提供了理论依据和技术基础;建立了舰艇并靠导弹补给及波浪补偿受控系统多体动力学,在补给舰和被补给舰随机运动下,在补给和波浪补偿系统作用下,应用多体系统离散时间传递矩阵法进行了补给系统动力学分析,得到了导弹补给过程中,波浪补偿时,导引电机和卷扬电机输入电机脉冲计算方法;建立了以PLC 控制系统为核心,用扭矩传感器测量导引带产生的扭矩来控制补给过程的控制方法;对系统振动问题进行了研究,提出了通过调整伺服电机参数减少系统振动的方法。

The main difficulty in maintaining the low-flying, right before the target stopped before there are some mountains, trees also more than the flying height, waiting for the alarm, flying low over the tree would die a hurry, here is a pattern even distracted skills tree from the woods and trees around the gap between the wearing, wearing a back end, failed several times, the requirements of high technology is,豁出去later, and is not even a few fighter planes like you play, the beginning fly, warning a short while, and soon the hills, two aircraft from put a red 4 missiles, missile thought more terrible, the result was even easy to flash, I saw a missile fly in front of the explosion really fun, in fact, the missile is a good hide, and more attention after the perspective to observe the missile position, when the missile away from you, almost 100 distance of 100 -200 m,(their estimate of the distance from there anyway) who has risen sharply and optional, you can play to stimulate the rapid decline in almost a sudden sharp rise in the ground, of course, elections are the rapid turn right turn left, air giant slalom, flip aircraft line, multi-练练, the computer is the point of missile小意思, nothing after playing air combat, interesting ah ~~~~ even the highest record was 28 to avoid a meeting, including surface-to-air missiles, the computer told me to fly by the tail I am thrown to the ground the trees the mountains 11 miles or a word and the computer novice and more air play than the simple low wear and more trees to the

难度主要在保持低空飞行,快到目标前有一些高山挡住,树还特别多,飞的比树高,等着报警把,飞的比树低想死着急,这里偶愣是用花样技巧,从树林里树与树的缝隙之间穿了过来,最后又穿了回去,失败几次,要求技术实在是高,后来豁出去了,不就是几架战斗机偶就跟你们玩玩,一开始就高飞,不一会报警了,快到山头, 2架飞机冲过来放了4导弹,原以为导弹多可怕,结果,被偶轻松闪过,看见导弹飞到我前面爆炸真好玩,其实导弹是很好躲的,注意多用后视角,观察导弹位置,当导弹离你差不多100-200米百距离,(自己估计的反正有段距离)可选者急速上升,还可以玩刺激急速下降快到地面时突然急速上升,当然选者急速右转左转,空中大回转,翻转飞机都行,多练练,电脑那点导弹完全是小意思,以后没事耍空战,有意思啊~~~~偶最高纪录是1次避了28枚导弹包括地对空,电脑跟我机尾飞被我甩在地上山上树上海里11次总之新手还是和电脑多玩玩空战比起超低空穿树简单的多的去了

Faced with the new operational environment, penetration of new technology, challenges, expeditions for many years,"Ticonderoga" class started a bit senile, inadequate, and until the U.S. guided missile cruiser CGX develop the next generation of service, the "Ticonderoga" class guided missile cruiser will also be faced with the fate of the stage of history.

面对新作战环境、新型突防技术的挑战,征战多年的&提康德罗加&级开始略嫌老态龙钟、力不从心,等到美国下一代CGX导弹巡洋舰研制服役后,&提康德罗加&级导弹巡洋舰也将面临着退出历史舞台的命运。

Under the definitions of the probability and the expected values of unhit attacking missile quantity,the expected values of anti-missile quantity and attacking missile quantity hit by a single anti-missile,the weapon operation efficiency was presented at various engagement pattern...

在定义未被命中的来袭导弹概率和数学期望、反导导弹数量的数学期望、单发反导导弹命中来袭导弹数学期望概念的基础上,研究不同作战方式下的武器作战效能。结果表明:提高导弹武器的效能,最为可行的方式是采用2发为单位的齐射。

PID control has been successfully used in many fields such as aviation, spaceflight, missile and other industry control system. The study object in the thesis is missile that flies hedgehopping over sea at minimum altitude. Many interference problem must be solved when missile flies at minimum altitude, otherwise the missile would be dangerous of bumping into the sea under the circumstances of bad weather and wave. The different kinds of interference factors are contradictions with requirements of control system, which can not be solved by PID control.

尽管在航空、航天、导弹以及其它工业控制领域PID控制曾经应用的十分普遍和成功,但对本文所研究的某型超低空掠海飞行的导弹,要实现超低空飞行必须处理好各种干扰问题,否则,在恶劣的气象和海情的条件下便有使导弹与海浪相撞的危险。

objective to evaluate the main points and complications of ct-guided percutaneous pneumocentesis in patients with lung lesions.methods cook 18~21g puncture needle was used to inserting aspiration in the optimal level,situs,angle and depth.and had made of multidrop.fifty-nine patients with lung lesions underwent ct-guided percutaneous pneumocentesis and follow-up.results the successful puncture rate was 100%,accurate diagnose rate was 92%(54/59).conclusion ct-guided pneumocentesis for chest lesion is a efficient and safe diagnostic method.but it is important to improve the doctor′s operating skill to lessen vascular complication.

目的 探讨ct引导下经皮肺穿刺活检的技术要点及并发症。方法采用cook公司18~21g自动弹射活检枪,选择最佳层面、进针点、进针角度和深度,行多点取材。回顾性分析59例肺内病变ct引导下经皮肺穿刺活检术。结果穿刺成功率100%,活检诊断准确率为92%(54/59)。3例发生轻度气胸,2例穿刺后咯血痰。结论 ct引导下经皮肺穿刺活检术成功率高,是安全的,但操作医生熟练的技术方法非常重要,并可以减少并发症的发生。

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