tactical air missile 中文意思是什麼
tactical air missile
解釋
戰術航空導彈-
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。 -
Abstract : based on the characteristic and tactical applications o f modern air strike weapons and according to the air - defense demand of naval ba se and coastal area, this paper analyzes the necessity and significance of devel oping air - defense missile patrol boat. the property and tactial applications of air - defense missile patrol boat are discribed too
文摘:從現代空襲兵器的性能和戰術運用特點出發，根據海軍基地及沿海地區對空防禦的需求，分析了發展防空導彈巡邏艇的必要性和重要性，並簡要分析說明了防空導彈巡邏艇的性能和戰術運用。 -
Based on the small tactical missile system design, an engineering method for ram - air servo system dynamic accuracy analysis and verifying unit design is put forward
摘要從小型戰術導彈總體設計的角度提出了一種繼電控制沖壓式伺服系統的動態精度和校正裝置的工程分析和設計方法。 -
Abstract : sins initial alignment error is one of the important error sources for tactical surface to air missile precision allocation. it is necessary and advantageous to research quickly separate technique of sins initial alignment error in outfield for improving missile guidance precision
文摘:捷聯慣性導航系統的初始對準誤差是戰術地空導彈精度分配中的主要誤差源之一，研究在外場條件下初始對準誤差的快速分離方法對于提高導彈制導精度具有積極意義。 -
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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