• This article is the third section to analysis effectiveness of the damage submunition against aircraft carrier.

    子母弹对航空母舰毁伤效果分析第三部分

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  • This is the second section about damage effectiveness analysis of aircraft carrier under the attacking of submunition.

    子母弹对航空母舰毁伤效果分析第二部分

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  • The structure principle of three line pendulum can be used to measure the moment of inertia of small missiles, submunition, aeroplane model and other structural members.

    利用线结构原理可以测量小型弹箭、子弹头、飞机模型其他构件惯性矩

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  • The result indicates that the damage effect of penetration submunition equipping the programmable electron time fuze meet the design requirement of undamaged areas of aerodrome runway.

    结果表明,由配用可编程电子时间引信彻子弹毁伤效果满足跑道未受损面积设计要求

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  • By using Particle Swarm Optimization (PSO), a model was built up for calculating the optimum dispersion height of intrusive submunition dispenser, and mathematical simulation was carried out.

    利用粒子优化算法建立侵彻子母弹最佳抛撒高度求解模型进行仿真计算。

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  • The dynamics model of parachute-munition system is used to analyze the motion characters of submunition under the effect of wind gust, and the calculation model of projective point is presented.

    利用伞-系统动力学模型,从工程应用角度出发,分析阵风小扰动作用子弹姿态运动特性,并以此基础给出修子弹弹下计算模型。

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  • The dynamics model of parachute-munition system is used to analyze the motion characters of submunition under the effect of wind gust, and the calculation model of projective point is presented.

    利用伞-系统动力学模型,从工程应用角度出发,分析阵风小扰动作用子弹姿态运动特性,并以此基础给出修子弹弹下计算模型。

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