• 简述了飞航导弹任务剖面、约束条件的给定、导弹的重量组成以及涡扇发动机模型。

    The mission section, the constrain conditions, the weight composition of the maneuverable missile, and the model of used in turbofan engine maneuverable missile were presented.

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  • 任务成功概率是任务成功性的概率度量,指在规定的任务剖面内,产品能完成规定任务的概率。

    Mission completion success probability means the weapon system to fulfill the probability its mission in a prescribe task profile.

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  • 该思路特点是首先进行与任务剖面相结合的可靠性评估试验,再对COTS器件进行可靠性筛选。

    Traits of the route were COTS 'reliability screening and COTS 'reliability evaluation test ahead of the screening, and the relationship between reliability technologies and mission profile.

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  • 结合作战任务剖面、导弹发射条件和弹道,设计出无人机防区外攻击导弹发射前、后的机动动作链。

    Due to mission profile , launched conditions and trajectory , maneuver chains for stand off missile are designed . instruction control model and maneuver model is setup for ucav flight simulation.

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  • 根据高超音速飞行器的特点,设计了高超音速飞行器的任务剖面,包括初始段、巡航段和末端攻击段。

    According to the characteristic of the hypersonic aircraft, the task of designing the hypersonic aircraft include initial phase, cruise phase and end attack phase.

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  • 对综合控制软件的任务剖面进行了分解,并给出了软件在系统测试与飞行试验阶段运行可靠度的计算方法。

    Then, based on the decomposition of task section plane of general missile control software, the procedures for the operational reliability .

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  • 为了获得优化的组合动力空天飞行器爬升轨迹,以一型水平起降空天运载飞行器为依托,针对任务剖面建立典型状态的飞行动力学模型。

    To acquire the climb track of Aero-Space Plane, it is established that the flight dynamics model of the Aero-Space Plane which takes off and lands.

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  • 文章对正在研制中的“自持式剖面循环探测漂流浮标”完成一个剖面测量任务的过程,进行了运动分析和数值计算。

    The whole working process of The Autonomous Profiling Drifter is described. Then the analysis of the drifter's moving and the numerical calculation are given.

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  • 文章对正在研制中的“自持式剖面循环探测漂流浮标”完成一个剖面测量任务的过程,进行了运动分析和数值计算。

    The whole working process of The Autonomous Profiling Drifter is described. Then the analysis of the drifter's moving and the numerical calculation are given.

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