terminal accuracy 中文意思是什麼
terminal accuracy
解釋
末端引導精度-
It is a more feasible method to realize the missile ’ s firing accuracy, by studying scene matching, track following, the middle guidance law and the terminal guidance law
比較可行的方法是抓住航跡規劃、航跡跟蹤、景象匹配、中制導和末制導等問題的研究，實現巡航導彈精確打擊目標。 -
Simulation result showed that response time of missile was reduced and guidance accuracy was accordingly increased by side jet and aerodynamic compound control manner in terminal guidance
通過模擬研究表明：在末制導階段，採用燃氣動力氣動力復合控制方式可提高導彈的快速性，進而提高導彈的制導控制精度。 -
Mortars provide integrated indirect fire support to the infantry, with quick response times, the ability to bring fire safely to within close range of friendly forces, good accuracy and range, and dramatic terminal effects
迫擊炮可為步兵提供綜合性的非直瞄炮火支援，反應迅速，可為友軍安全提供近距離炮火支援，射程適中，打擊準確，效果直接。 -
By means of the step control of pmsm, it can offer accurate and reliable position control for the angle travel terminal equipment. step angle is small, torque is large and inertia is small. this system will promote the technical guideline and control accuracy of the flow and pressure control
利用永磁同步電動機的步進控制，為角行程終端設備提供準確可靠的定位控制，步進角小、轉矩大、慣量小，將使流量及壓力控制達到高的技術指標和控制精度。 -
Based on analyzing the mechanism of direction finding triangulation location and location accuracy for two - ship passive locating, the acquisition probability model of anti ship missile terminal guidance radar is presented for two - ship passive locating : and the effects of the key factors to the probability are analyzed, and then the primary factors are pointed not by analyzing the results in different conditions
摘要首先簡要介紹了無源定位技術，然後著重分析了雙艦無源測向交叉定位以及其誤差產生的機理，在此基礎上，給出了雙艦無源定位情況下實施超視距攻擊時，反艦導彈末制導雷達開機時刻對目標的捕捉概率模型，並通過模擬分析雙艦距離。 -
In order to simulating rapidly and analyzing the dynamic behavior of the whole mems but not reducing accuracy significantly, the terminal behavior of multi - terminal components was modeled as reduced - order model ( or called macromodel ). upon the finite element model theory micro - mechanical devices or components were modeled in the spatial, which afforded theoretic foundation and technical support to mems system - level design
為了便於在不顯著影響精度而能快速地模擬與分析mems整個系統動態行為，通過器件或組件的降階模型（或稱為宏模型）方法描述了多埠組件的埠行為，並採用有限元模型理論在三維空間內建立了微機械器件或組件宏模型，為系統級設計所需要的組件庫的建立提供了理論基礎和技術支持。 -
The merits of single terminal fault location are its reliability and its accuracy is n ' t affected by the type of line, fault resistance and two sides systems theoretically but this method has problems such as the identification of reflection wave and the unidentifiable area of reflection nearby which are research purpose and core of this paper
單端行波故障測距方法的優點是其可靠性和精度在理論上不受線路類型、故障電阻及兩側系統的影響，但單端行波故障測距方法存在反射波的識別問題，且在近區還存在無法識別反射波區域。這就是本文的研究目的和中心。 -
The tactical missile seeker handover accuracy from midcourse to terminal guidance is researched. the small perturbation method is proposed to analyse error sensitivity of the seeker presetting parameters from error sources. firstly, the terminal guidance seeker presetting parameters are computed, based on the equations of a surface - to - air missile movement and a target movement. then the seeker presetting unaccuracy due to the command guidance radar measurement errors is also computed. it can be seen that the seeker presetting errors increase rapidly when the missile is close to the target, which leads to an important conclusion that the late seeker handover from midcourse to teminal guidance should be avoided
研究復合制導的戰術導彈中末制導交班的導引頭預定精度問題.提出用小擾動法分析導引頭預定參數對誤差源的誤差敏感性關系.以中遠程防空導彈為例，結合導彈運動方程組和目標運動模型，計算了中末制導交班的導引頭預定參數，並計算了在制導站雷達測量誤差下的末制導導引頭預定參數的計算精度.可知，導引頭定位參數的計算誤差隨著彈目距離的接近而顯著增大，得到中末制導交班不能太晚的重要結論 -
Abstract : the tactical missile seeker handover accuracy from midcourse to terminal guidance is researched. the small perturbation method is proposed to analyse error sensitivity of the seeker presetting parameters from error sources. firstly, the terminal guidance seeker presetting parameters are computed, based on the equations of a surface - to - air missile movement and a target movement. then the seeker presetting unaccuracy due to the command guidance radar measurement errors is also computed. it can be seen that the seeker presetting errors increase rapidly when the missile is close to the target, which leads to an important conclusion that the late seeker handover from midcourse to teminal guidance should be avoided
文摘:研究復合制導的戰術導彈中末制導交班的導引頭預定精度問題.提出用小擾動法分析導引頭預定參數對誤差源的誤差敏感性關系.以中遠程防空導彈為例，結合導彈運動方程組和目標運動模型，計算了中末制導交班的導引頭預定參數，並計算了在制導站雷達測量誤差下的末制導導引頭預定參數的計算精度.可知，導引頭定位參數的計算誤差隨著彈目距離的接近而顯著增大，得到中末制導交班不能太晚的重要結論
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