空地導彈 的英文怎麼說

中文拼音 [kōngdedǎodàn]
空地導彈 英文
air-to-ground mi ile （agm）
  • 空 : 空Ⅰ形容詞（不包含什麼; 裏面沒有東西或沒有內容; 不切實際的） empty; hollow; void Ⅱ名詞1 （天空） s...
  • 導 : 動詞1. （引導） lead; guide 2. （傳導） transmit; conduct 3. （開導） instruct; teach; give guidance to
  • 彈 : 彈名詞1. （彈子; 小球形的東西） ball; pellet 2. （內裝爆炸物, 具有破壞和殺傷能力的東西） bullet; bomb
  • 空地 : opening; blank; area; lawn; maidan; vacant lot; open ground; open space
  • 導彈 : guided missile
  1. Then analyses the effectiveness of air - raid firepower of us carrier battle group at four sections

    進而分別建立了機載普通對地攻擊彈藥和巡航導彈、空地導彈對地面目標的毀傷能力的模型。
  2. Analysis of air - to - ground missile countermine simulation system based on uml

    的空地導彈攻防對抗模擬系統研究
  3. Analyzing to a stand off missile ' s flight characteristics, the as missile trajectory simulation is completed

    在分析了典型防區外導彈飛行特點的基礎上，進行空地導彈彈道模擬。
  4. A calculation model of minimum launch range for air to ground missile

    空地導彈最小射程的一種估計方法
  5. Research on the damage potential of tv - command - guided air - to - ground missiles

    電視指令制導空地導彈對目標的毀傷性能研究
  6. Research on the vertical intercept terminal guidance system of tv - command - guidance air - to - ground missile

    電視指令制導空地導彈垂直命中目標的末制導系統研究
  7. Study on idss of multiple tube launcher rocket system

    對電視制導空地導彈巡航飛行高度的分析
  8. Matlab - based dynamic simulation of tv - guided air - to - surface missile

    的電視制導空地導彈動態模擬
  9. Sensitivity of guidance error of tv - guided missile based on orthogonal experiments

    基於正交試驗的電視制導空地導彈制導誤差靈敏度分析
  10. Through those models, ucav representative maneuver chains simulation in as attack is achieved. a simulation is carried out for ucav stand off attack, through which, the corporation between ucav and as missile is discussed

    通過一個無人機實施防區外攻擊的算例，總結出導彈發射前後無人機的動作鏈特點，對無人機作為空地武器發射平臺與空地導彈的配合問題進行了初步的探討。
  11. 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。
  12. Analysis and simulation for guide precision of air - to - surface missile

    空地導彈制導精度分析及模擬
  13. Simulated software of air - surface missile damaging the targets on the ground

    空地導彈毀傷地面目標計算機模擬軟體
  14. Research on the algorithm about damages of air - to - surface missile attacking target

    空地導彈對目標的毀傷性演算法研究
  15. Damaging evaluation of air to surface missile against mobile mi ssile armament system

    空地導彈對機動導彈武器系統毀傷能力評估
  16. 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。
  17. 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。
  18. In this paper, the design technical management and synthesis of engineering specialty in each stage of airplane life span is discussed emphasisly, in the light of the development of a certain medium - range aifto - ground missile bomber and a certain air4o - ship missile bomber. the principle and method of engineering system engineering is adopted to the management of airplane design technique. by drawing on the experience of advanced management from foreign airplane ' s abstract development, the standardized method of the design technical management and synthesis of engineering specialty in each stage of airplane life span is presented in this paper

    本文結合某型中程空地導彈機和某型空艦導彈機不同階段的研製，對飛機壽命周期各階段設計技術管理和工程專業的綜合進行了重點研究，把工程系統工程的原理和方法應用到飛機設計技術管理中，借鑒了國外飛機研製的先進管理方法，提出了飛機壽命周期各階段設計技術管理和工程專業綜合的規范化方法。
  19. Based on optimal control theory and singularly perturbed theory, a singularly perturbed midcourse guidance law that guarantees air - to - ground missiles to ascent quickly is proposed. this new guidance law is a composite control law consisting of three parts : optimal climbing control using variable weighting factor method, minimum energy cruising phase control and minimum energy switching phase control. moreover, a new control logic is designed in order to remove influence of climbing control on switching phase. simulation results of a certain type of air - to - ground missile are presents. it is shown that, with simple control algorithm and feasible onboard implementation, this law not only guarantees air - to - ground missiles to ascent quickly, but also satisfies the requirements of midcourse phases. the studies have important theoretical meaning and great value of engineering application

    為滿足實際作戰的要求，基於最優控制理論和奇異攝動方法，提出了一種可保證中遠程空地導彈快速爬升到最優高度的中制導律.它由變系數最優爬升控制，最小能量巡航控制和最小能量下滑控制組成.為了減小爬升段控制對下滑段的影響，提出了一種新的控制邏輯.最後針對某型空地導彈進行了模擬.結果表明，該中制導律較好地滿足了中遠程空地導彈在中制導段的要求.本文的研究結果具有較好地工程參考價值
  20. Abstract : based on optimal control theory and singularly perturbed theory, a singularly perturbed midcourse guidance law that guarantees air - to - ground missiles to ascent quickly is proposed. this new guidance law is a composite control law consisting of three parts : optimal climbing control using variable weighting factor method, minimum energy cruising phase control and minimum energy switching phase control. moreover, a new control logic is designed in order to remove influence of climbing control on switching phase. simulation results of a certain type of air - to - ground missile are presents. it is shown that, with simple control algorithm and feasible onboard implementation, this law not only guarantees air - to - ground missiles to ascent quickly, but also satisfies the requirements of midcourse phases. the studies have important theoretical meaning and great value of engineering application

    文摘:為滿足實際作戰的要求，基於最優控制理論和奇異攝動方法，提出了一種可保證中遠程空地導彈快速爬升到最優高度的中制導律.它由變系數最優爬升控制，最小能量巡航控制和最小能量下滑控制組成.為了減小爬升段控制對下滑段的影響，提出了一種新的控制邏輯.最後針對某型空地導彈進行了模擬.結果表明，該中制導律較好地滿足了中遠程空地導彈在中制導段的要求.本文的研究結果具有較好地工程參考價值
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