target missile 中文意思是什麼
target missile
解釋
靶標導彈-
For quick truning to target of air - to - air missile ( aam ) for short range dogfight in large off - boresight it is necessary to study the agile turn control law
摘要為了使近距格鬥空空導彈在大離軸角發射時能快速地轉向目標，需要研究快速轉彎控制律。 -
For all practical purposes a ballistic missile such as atlas is guided to its target.
根據各種實用目的，可使象「阿特拉斯」這樣的彈道導彈導向其目標。 -
As we all known, the ballistic trajectory is a pilotless missile, which loads rocket engine and control system, these will drop the missile to the target along its ballistic
眾所周知，彈道導彈是一種無人駕駛的飛行器，它裝有火箭發動機和控制系統，其目的是把導彈沿一定的彈道送到目標區。 -
A guided missile is one which is usually fired in a direction approximately towards the target.
通常導彈是大致對著目標方向發射的。 -
The last part of this paper designed a simple three - dimensional proportion homing rule according to three - dimensional opposite equation of motion of missile - target. and the simulation of the big - loop of terminal guide, control and motion was given
最後根據導彈?目標的三維相對運動方程設計了一種簡單的末端三維比例制導律，並對導彈的末制導、控制以及運動大迴路進行了綜合模擬。 -
The importance of collision course in guidance of homing missiles is elaborated, that is, the sufficient and necessary condition for a successful interception is the missile and target in the collision course
闡述了碰撞過程在尋的制導中的重要意義，即實現攔截的充分必要條件是導彈與目標處于碰撞過程上。 -
Unless the target starts manoeuvring, the missile tends to fly straight near interception.
除非目標開始移動，否則導彈會直線地飛行接近碰撞點。 -
Research on separation sequence of mirv missile based on target attacking sequence
基於目標打擊順序的多彈頭導彈分導方法 -
Since the target glint is essentially a very low frequency phenomenon whose bandwidth is typically equal to or less than that of the system, it is difficult for a missile to filter it out, or will cause the miss to increase
由於目標閃爍的頻率通常小於或者與系統的頻帶相當，所以導彈無法濾掉此干擾信息，致使系統脫靶量增大。 -
The anti - cruise missile system is a fire - control system, which is developed by a military factory and our lab. the assistant of firepowers disposal is the sub - system of anti - cruise missile system. it analyse the information of target protected, digital maps and the rules of enemy ` s activities to provide a optimized solution of disposals of our firepower. and also it provide plenary man - machine conversations to adjust the solution. before this system, for the purpose of firepower disposal, commanders must be autoptical to disposal, it takes long terms, and is not optimized and it has no convenience to adjust the disposal
陸軍防空兵反巡航導彈系統是某軍工廠和我們教研室合作研製的火力控制系統。輔助部陣是其中的一個子系統，它通過分析戰區地圖數據及保衛目標信息，敵方活動規律，並且提供充分的人機交互，對己方的火力點布置進行優化指派。它在戰前為己方防空部隊提供一個隊形布置的解決方案。 -
Second, by computing the trajectory of the missile and the method of analyzing cep, influences that the fighter ' s height, speed, pitch angle, the deflection angle between fighter and target, and the target moving characters make on the times of fighter attack and missile launch are deeply developed. third, by relating the motion of the missile and the fighter, the influences that fighter ' s dive angle and the deflection angle between fighter and target make on the attack field of the fighter are discussed in this paper when the fighter perform vertical and horizontal attack. criterion of attack effect is proposed focusing on attack time of the fighter, trajectory of the missile and destruction probability to the target
本文主要完成了以下幾個方面的工作：對導彈可發射區和飛機可攻擊區進行建模，通過對導彈彈道的模擬計算，並運用典型的圓概率偏差精度分析方法，詳細討論了飛機實施攻擊時，飛機的飛行高度h 、速度v 、俯仰角、與目標的偏離角_ x及目標運動特性等對飛機攻擊時機和導彈發射時機的影響；因此，將飛機和導彈結合起來，詳細研究了飛機在垂直平面和水平平面內實施攻擊時，飛機俯沖角和與目標的偏離角_ x對飛機的攻擊范圍的影響；以飛機實施攻擊的時間t 、彈道特性和對目標的殺傷概率p來評判對地攻擊的效果；最後給出典型算例，通過對空地攻擊過程的模擬實現，對飛機飛行過載提出要求。 -
This design method overcomes the traditional autopilot ' s disadvantage that should shift the autopilot ' s gain according to flight phase ; it also can make the btt missile fly stably along the whole trajectory, and can intercept a maneuvering target accurately
該設計方法克服了傳統自動駕駛儀在控制導彈飛行中需逐段切換增益的不足，能控制btt導彈在大空域內沿全彈道穩定飛行，並能精確攔截機動目標。 -
Appropriate evaluation indexes are established based on the considerations for the missile impact, the target tracking stability and the flight stability of the missile. a simulation program is designed to simulate the missile - ship engagement scenario, and also evaluate the electronic protection capability of the active - passive multimode seeker
分別從反艦導彈彈著點、導引頭目標跟蹤穩定性和反艦導彈飛行穩定性三個方面考慮，研究了評估復合制導反艦導彈主被動復合導引頭抗干擾性能的基本理論和方法，建立了評估指標。 -
The calculation model for killing probability of fragmentation warhead of missile to air target
導彈破片戰斗部對空中目標的殺傷概率計算 -
In the family of precisely guided weapons, tv - guided weapon system is one of the widely used precise guided weapons. tv - guided weapon system is based on image processing, automatic control and information science. it extracts the location information of missile image from tv image, and guides the missile to attack the target
電視制導武器系統是廣泛投入實戰應用的精確制導武器之一，它將圖像處理、自動控制、信息科學有機地結合起來，從電視圖像信號中提取導彈位置信息並導引導彈擊向目標。 -
A homing head is merely a target tracker; when mounted in an airborne missile it is sometimes called a "homing eye" or a "seeker".
導引頭是一個目標跟蹤裝置，當它被裝在導彈上時，有射稱之為「尋的器」或「探尋器」。 -
A homing head is merely a target tracker ; when mounted in an airborne missile it is sometimes called a " homing eye " or a " seeker "
導引頭是一個目標跟蹤裝置，當它被裝在導彈上時，有射稱之為「尋的器」或「探尋器」 。 -
Advantages, disadvantages and limits of arm are thoroughly examined using signal processing methods. based on the above, incoherent and coherent two - point - source decoy methods and modified coherent two - point - source decoy methods to deflect arm are brought forward. arm ’ s homing heads are generally of mono - pulse structure, so coherent two - point - source ’ s interference resembles that to mono - pulse radar except that interference to radar belongs to far field scope, but interference to arm varies from far field to near field because relative distance drastically changes between the homing head and the two - point - source with missile ’ s homing head continually approaching the target
Arm的導引頭一般為單脈沖體制，因此，相干兩點源對導引頭的干擾類同於對單脈沖雷達的干擾，不同的是:對雷達的干擾都是遠場，而導引頭隨著導彈不斷接近目標，兩點源與導引頭的相對位置發生劇烈變化，由遠場變化到近場;導引頭天線口面上的合成場也發生了大的變化，相位波前的畸變產生干擾，這就是相干兩點源誘偏的基本思想。 -
Shack on the target - missile lock on a aircraft
目標閉入-敵飛機進入本機飛彈照準范圍並被鎖定 -
Study on hit criterion of explosively formed projectiles to target missile
攻擊單元與目標交匯準則的研究
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