ground missile 中文意思是什麼
ground missile
解釋
地面試驗的導彈-
Agm air to ground missile
空對地導彈 -
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 -
At present, a datum plane - conversion scheme is introduced in the sight system of active ground - to - ground missile. in this scheme the datum plane of sight system is transferred from inertia combination to missile terminal, and the angle of two datum planes is measured at the technical position
目前，常規導彈在瞄準中採用了基面轉換方案，將導彈瞄準基面由慣性組合轉換到彈體尾段，兩基面夾角在技術陣地測量。 -
As the popularization and application of integrate logistics support engineering thinking at our country industry field and the military continuously, the evaluation of equipment integrate logistics support capability become the mostly means to check up the stand and fall of equipment character of supportable design, the efficiency of the equipment using supportability and the decision - making to equipment ' s continuous model development, at the same time, along with the development and maturity of computer simulation technique, the research of analysing and evaluating equipment ' s effectiveness steps into a new stage, we can get the handle and maintain data on the base of originally lasting accumulating in existence by utilizing the computer emulating technique, which is necessary to analyzing and evaluating the ground - to - ground missile ' s integrate logistics support effectiveness, via simulating the handling and maintaining process of ground - to - ground missile weapon, we can evaluate the ils effectiveness comp rehensively, impersonally, veraciously, consequently, provide decision - making gist to make the best support project
隨著綜合保障工程思想在我國工業界和軍方不斷普及和推廣應用，裝備綜合保障能力的評估成為檢驗裝備保障性設計好壞、裝備使用保障效能高低以及裝備后續型號發展決策的主要手段，同時隨著計算機模擬技術的不斷完善和成熟，裝備效能分析與評估研究進入了一個新階段，我們可以在導彈武器綜合保障效能分析與評估所需使用與維修數據原始積累的基礎上，利用計算機模擬導彈武器在真實使用環境中的使用維修過程，達到對導彈武器系統的綜合保障能力進行更全面、客觀、準確的評價目的，從而為裝備保障部門制定最優的保障方案提供更好的決策依據。 -
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 -
Trajectory planning of the television - guided and air - to - ground missile
水下彈丸速度擬合方法的誤差分析 -
A new method about aiming azimuth checking before launch of the ground - to - ground missile
一種基於遙測信息的瞄準方位角檢查方法 -
Ground - to - ground missile
地地導彈 -
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 -
Air - to - ground missile ( agm ) provides intuitionistic observation plat for agm tactical application and coordinated operation
開發的空對地導彈三維動畫系統為空對地導彈的戰術應用、協調作戰提供了直觀的觀察平臺。 -
Using the theory of virtual reality we develop the system of engine testing and the system of air - to - ground missile ( agm ) in vc + +
在vc + +環境中，利用虛擬現實的原理設計開發了發動機試車三維動畫系統和空對地導彈三維動畫系統。 -
The first chapter introduced the background of researching problem, presents a common process to resolve this kinds of problem and a common procedure for this method ; the second chapter briefly presented the basic thinking of equipment ils engineering and equipment technique support, discriminate between equipment ils and equipment technique support ; in chapter 3, we studied the basic configuration of tactics ground - to - ground missile weapon system and the work content of technique support thoroughly, established the work - flow model of tactics ground - to - ground missile technique support in combat environment ; in chapter 4, we mostly discussed the essence content of technique support evaluation, introduced the application of tradition static evaluating methods in the aspect of evaluating the capability of tactics ground - to - ground missile technique support, such as ahp, adc and synthesis fuzzy evaluation method, and put forward the method of computer dynamic simulating evaluation ; the fifth chapter particularly introduced the design thinking and realizing method of tactics ground - to - ground missile technique support evaluation by computer dynamic simulating, in the end, give an emulation realization instance
第二章對裝備綜合保障工程和裝備技術保障基本思想進行了簡要介紹，並對裝備綜合保障和技術保障進行了辨析。第三章對地地戰術導彈武器的基本結構、技術保障工作內容進行了深入的分析研究，建立了地地戰術導彈戰時技術保障工作流程模型。第四章探討了地地戰術導彈技術保障評估的基本內容，詳細介紹了諸如「 adc 」 、綜合模糊評判等傳統評估方法在地地戰術導彈技術保障能力評估方面的應用，提出了計算機動態模擬評估的方法，並對地地戰術導彈技術保障能力動態模擬評估進行了初步分析。 -
This paper principally discusses the problem of technique support effectiveness evaluation of tactics ground - to - ground ground - to - ground missile which is in serve. discusses the applications of some evaluation means in tactics ground - to - ground missile technique support evaluation, and on the base of analyzing and investigating the tactics ground - to - ground missile weapon system ' s basic configuration and technique support evaluative content and technique support work - flow in combat environment, simulate and evaluate the capability of technique support
本文主要論述了使用階段地地戰術導彈技術保障能力模擬評估問題，同時對一些傳統的裝備效能評估方法在地地戰術導彈技術保障能力評估方面的應用進行了初步探討，並在對地地戰術導彈武器基本結構、技術保障評估內容以及戰時地地戰術導彈技術保障基本工作流程進行全面分析的基礎上，對戰時地地戰術導彈技術保障能力進行了模擬評估。 -
Anti - radiation missile ( arm ) is an air - to - air or air - to - ground missile that can seek, track and destroy radar systems by making use of electromagnetic wave of the radar beaming, which is also called anti - radar missile
反輻射導彈（ anti - radiation - missile ， arm ）是一種利用雷達輻射源發射的電磁波，發現、跟蹤並摧毀雷達系統的空空、空地機載導彈，也稱為反雷達導彈。 -
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。 -
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。 -
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 -
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 -
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。
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