应用动态逆和三时标分离的飞航导弹过载控制离散化设计
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应用鲁棒动态逆和三时标分离的飞航导弹过载控制系统设计
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methods to deal with constraints in overload control systems of winged missile
飞航导弹过载控制系统中约束条件的处理方法
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research on technology in evaluation-decision of conceptual design for winged missile
飞航导弹总体方案评价决策技术研究
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anti-jamming communication design of guidance system and control system in winged missile
飞航导弹导引头系统与控制系统抗干扰通讯设计
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the velocity information fusion's research of winged missile based on least square method
基于最小二乘法的飞航导弹速度信息融合研究
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与空气动力有翼导弹大不相同,一枚真正的弹道导弹只在起飞的几分钟内受人们控制。2.It proved that winged vehicle could exist alone in space.它证明了有翼飞行器能够单独在太空中飞行。3.The experimental research of winged vehicle for dynamic aerodynamic characteristics at high speeds有翼航天飞行器高速动态气动特性试验研究
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