兵工自动化
兵工自動化
병공자동화
ORDNANCE INDUSTRY AUTOMATION
2009年
8期
18-20
,共3页
末制导%俯冲落角%飞行高度%飞行速度
末製導%俯遲落角%飛行高度%飛行速度
말제도%부충락각%비행고도%비행속도
Terminal guidance%Angle of dive%Altitude of Flight%Speed of Flight
制导性能直接影响命中目标的精度.以某型飞航式成像制导武器为研究对象,研究影响末制导性能的关键因素-俯冲落角、末端飞行高度以及末端飞行速度,并对其进行理论分析,得出相关因素与末制导性能之间的关系,同时进行数据仿真,为设计出符合该型制导武器气动特性的末制导航迹提供理论依据.
製導性能直接影響命中目標的精度.以某型飛航式成像製導武器為研究對象,研究影響末製導性能的關鍵因素-俯遲落角、末耑飛行高度以及末耑飛行速度,併對其進行理論分析,得齣相關因素與末製導性能之間的關繫,同時進行數據倣真,為設計齣符閤該型製導武器氣動特性的末製導航跡提供理論依據.
제도성능직접영향명중목표적정도.이모형비항식성상제도무기위연구대상,연구영향말제도성능적관건인소-부충락각、말단비행고도이급말단비행속도,병대기진행이론분석,득출상관인소여말제도성능지간적관계,동시진행수거방진,위설계출부합해형제도무기기동특성적말제도항적제공이론의거.
Performance of guidance directly influences the accuracy of target attack. Make a certain type of imaging-guided flight weapon as the object, research major factors that affect terminal guidance performance--angle of dive, terminal flight altitude and terminal flight speed and make theoretic analysis on these factors, thus achieve relations between factors and terminal guidance performance. Meanwhile, proceed data simulation, and provide theoretic reference for terminal guidance tracks of guided weapons with aerodynamic characteristics of the given type.