air-to-air missile attack 中文意思是什麼
air-to-air missile attack
解釋
空對空導彈攻擊-
The software designed for the system is validated by experiments and proved correct. the system can s imulate the real air - stream and put it on missile ' s wings to make them work under the same force environment as the real spread process, so the relationship of explosive stuff and attack angle can be calculated
本文所設計的監控軟體已通過實際系統的驗證，說明整個系統的設計是合理正確的，能夠真實的模擬力矩，產生一種類似真實氣流阻力的載荷，並將其正確施加於彈翼（尾翼）上，使彈翼（尾翼）能在與展開過程中實際受力相同的狀態下工作。 -
Simulation of standoff land air - to - ground anti - radiation missile attack ' s zone and its combat effectiveness
防區外空地反輻射導彈攻擊區及作戰效能模擬 -
The traditional air defense system which detect and attack targets only depend on ordinarily radar was in an exceedingly passive position and difficult to ward off blows when the cruise missile was used in war
它的出現使得傳統的僅僅依靠普通雷達探測目標和引導武器射擊目標的防空系統處于極端被動和難以招架的局面。 -
The air - defense troop especially the ground - to - air troop must fight in its position, and the correct disposition and position choice of the ground - to - air missile troop or not is an important factor that the battle to anti - shot the air - attack validity or not, the disposition and position choice of the ground - to - air missile troop need to cinsider some terms synthetically such as geography, mobilization and fighting - time factors ect
摘要防空部隊特別是地空導彈部隊抗擊敵空襲作戰必須依託相應的陣地進行，而地空導彈部隊陣地部署與選擇的正確與否是地空導彈部隊能否有效進行抗擊敵空襲作戰的一個重要因素，地空導彈部隊陣地部署與選擇需要綜合考慮地形條件、機動條件、作戰時間條件等各種因素。 -
For missile, either strategical or tractical, the most important thing is to attack the target accurately. this depends upon the accurate location of the larget by the missile radar. for protecting radar antenna from external environment and for air - dynamical requirement, a radome is used to enclose the antenna. but the radome interferes in the orientation of the antenna, degradaties its perfor - mance, decreases the power reaching the target, and most importantly, it produces so called boresight error ( bse ) that is, makes the antenna shows a slightly different direction of the target from its true direction, the boresight error is define as the angle shifted, and the boresight error slope ( bses ) is defined as the ratio of angle shift to the tracing angle of the radar antenna. to predict the boresight error and boresight error slope is an unavoiding chief task in designing radome and in its operation
在戰略和戰術雷達制導導彈中，一項重要的工作就是對目標的準確跟蹤，這取決于導彈雷達對目標的準確定位。為了保護雷達天線不受外界環境的影響，天線罩被應用進來，但天線罩在保護天線不受外界惡劣環境影響的同時對天線電磁輻射產生某些干擾，使天線的電氣性能降低，影響天線的功率傳輸，更重要的是產生瞄準誤差。它使目標的視在位置與真實位置有一個角度差，這個角度差就是天線罩的瞄準誤差。 -
The paper mainly does research on simulation of the air - to - surface ( as ) attack mission. on the basis of that, as attack representative maneuver chains are designed. and, corporation between uninhabited combat air vehicle ( ucav ) and as missile is discussed in the process
本文主要針對無人機對地攻擊任務特點，開展模擬模型研究，並以此為基礎設計出無人機防區外攻擊的典型動作鏈，對攻擊過程中無人機與空地導彈的配合問題進行了初步的研究。 -
Fourthly, we discuss and simulate the transformation method of relative parameters of ground target based on data link. and then we analyze decision algorithm of air - to - ground attack. especially, we educe three dimensional terminal guidance law of air - to - ground missile in the disturbance of wind, and give the simulation result
本文也研究了空對地攻擊的若干技術，包括對獲得數據鏈指揮下地面目標相對于某攻擊機當前時刻相關參數的方法進行了闡述及模擬，並在此基礎上討論了單機對地面多個目標的攻擊決策演算法，同時提出了一種風干擾下空地導彈的三維末制導導引律，且利用數字模擬進行了驗證，並指出研究空地導彈導引律時考慮風影響的必要性。 -
Then according to system simulation technology, the overall air - to - ground attack simulation plan is made with the thought of models and layers. after that, the mathematical models of main parts in the simulation are made such as aircraft body, propulsive system, flight control system, fire control system, bomb and air - to - ground missile. on the basis of these mathematical models, using the object - oriented design methodology, a set of air - to - ground attack real - time visual simulation software is developed. this software can be used to aid aircraft design, research of air - to - ground attack tactics and flight training
本文首先介紹了現代戰爭中空對地攻擊的技術裝備及其特點，計算機模擬技術的發展以及面向對象的軟體設計思想；而後使用系統模擬技術，依據分層、模塊化設計思想，制定了空對地攻擊模擬系統總體設計方案；之後根據目前技術狀況，建立了戰斗機機體、推進系統、飛控系統、火控系統、航空炸彈、空地導彈等子系統數學模型；在此基礎上，利用面向對象的軟體設計思想，在基於pc的平臺上開發了一套對地攻擊視景模擬軟體，實現了戰斗機對地攻擊實時視景模擬。 -
Then we simulated the result of air - to - air missile attack using matlab
並使用matlab對某型空空導彈攻擊過程進行了模擬。 -
The load control system has already passed the test ' s validate. it shows that the design of whole system is correct. the system can truly simulate the real air - stream and put it on missile ' s wings to make them work on the same force situation as in the real spread process, so the relationship of explosive stuff and attack angle can be confirmed
本文所設計的加載控制系統已通過實際系統的驗證，說明整個系統的設計是合理正確的，它能夠真實地模擬類似真實氣流阻力的載荷，並施加於彈翼或尾翼，模擬其在真實工作環境下的受力狀態，可以測算導彈攻角與火工品填藥量的關系。 -
The mission it was designed for was to penetrate thick soviet air defenses in central europe and attack key targets and air defense systems ( radars, command centers, and missile launchers )
其任務是突入蘇聯在中歐的嚴密的防空體系，對重要目標和防空系統（雷達、指揮中心和導彈發射架）實施攻擊。 -
Then we analyzed the change process of trajectory in air - to - ground missile attack, built the movement equations based on the center of gravity of every segment. in the end we gave the whole trajectory simulation result of air - to - ground attack
分析了空地導彈攻擊的彈道變化過程，將攻擊過程劃分為五部分，分別對各段建立了重心運動方程並進行了模擬，最後給出了空地導彈攻擊的全過程彈道模擬結果。 -
In order to win the war in the future and carry out the energetically defensive strategic principle, we must adopt effective measures and build the integrated defensive system to deal with cruise missile, which is seasoned with the fertility foundation, science and technology development level and economic strength of our country. so long as this, we can mop the floor with precision guidance cruise missile as the nucleus of the enemy ' s air attack, progressively try to gain the war ' s initiative and win the war finally
要在未來打贏這類現代戰爭，並貫徹積極防禦的戰略方針，必須採取有效措施，建立適應于國家生產力基礎、科技發展水平和經濟實力的反巡航導彈綜合防禦系統，徹底粉碎敵方以精確制導巡航導彈為核心的空中打擊，才有可能逐步掌握戰爭主動權，奪取戰爭的最後勝利。 -
The designed robust guidance laws are used to the simulation of air - air missile ' s attack process. the designed robust guidance laws are more valid than the proportional navigation guidance law
與傳統的比例制導律相比，所設計的h 』魯棒制導律效果更好，魯棒性更強。
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