作 者: (唐小平); (李智军); (胡龙兵); (胡牡丹); (安贵乾); (孙栋梁);
机构地区: 航空工业洪都,江西南昌330024
出 处: 《教练机》 2017年第2期35-38,共4页
摘 要: 基于察打一体无人机,针对平台定常盘旋机动模型,推导了盘旋角、机目视线角、框架角、盘旋半径和锁定目标时刻机目水平距离间的关系,可为平台机动条件下武器发射窗口的分析计算提供参考。 According to the model of reconnaissance and strike integrated UAV’ S hovering, this thesis derives thehovering angle, the Line Of Sight (LOS)angle, the frame angle, hovering radius and the horizontal distance of aircraftand the locked target during locking target, which can provide reference to calculation and analysis of the launchingwindow for short-range air-to-ground missiles.