1、

Discrete-time overload control design for winged missile using dynamic inversion and three time-scale separation

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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2、

accuracy evaluation of electromagnetic scattering characteristic on winged missile in resonance region

飞航导弹谐振区电磁散射特性的精确预估

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3、

overload control system design for winged missile using robust dynamic inversion and three time-scale separation

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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4、

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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5、

overload control for winged missile using intelligent resistance

采用智能阻尼的飞航导弹过载控制

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6、

aerodynamic characteristics of winged missile

有翼导弹空气动力特性

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7、

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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8、

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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9、

design of sliding mode controller for an agile winged missile

高性能飞航导弹的一种滑模控制器设计

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10、

simulation software of integrated guidance for long-range winged missile

远程飞航导弹组合制导仿真软件

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11、

the analysis on dynamical stability of winged missile

有翼导弹的动态稳定性分析

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12、

laser weapon and defense techniques of winged missile

激光武器及飞航导弹的防护技术

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13、

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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14、

in contrast to the aerodynamic winged vehicle, a true ballistic missile is controlled for only a few minutes at the start of its flight.

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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