maneuverable missile 中文意思是什麼
maneuverable missile
解釋
機動導彈- maneuverable : 便於駕駛的
- missile : n 投射器；飛射器[箭、炮彈等]，射彈，飛彈；導彈。 an air to air （guided） missile 空對空飛彈，機...
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The empty weight to total weight ratio of subsonic maneuverable missile was given experimentally
利用經驗的預測方法對亞聲速飛航導彈的空重比進行預測。 -
By using the method of aircraft and turbofan engine integrated analysis, a model of maneuverable missile and turbofan engine integrated constrain analysis and mission analysis was developed and the computative examples and the analysis were given
摘要利用飛機渦扇發動機一體化設計的思路，建立了飛航導彈渦扇發動機一體化設計的約束分析和任務分析模型並給出了算例和分析。 -
The performance of next generation maneuverable missile was predicted by taking into account its important parameters such as lift to drag ratio, empty weight to total weight ratio and effective load
在考慮導彈空重、有效載荷和氣動特性的情況下，預測了未來先進飛航導彈的性能。 -
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
簡述了飛航導彈任務剖面、約束條件的給定、導彈的重量組成以及渦扇發動機模型。 -
The cycle parameters of missile for turbofan engine were optimized for meeting the demand of maneuverable missile, and the developing trend of missile for turbofan engine was predicted
根據飛航導彈的要求對渦扇發動機進行了循環參數優化選擇並預測了未來渦扇發動機的發展趨勢。 -
By using the method of aircraft and turbofan engine integrated analysis, a model of maneuverable missile and turbofan engine integrated optimum design was developed and the computational examples and the analysis were presented
摘要利用飛機渦扇發動機一體化設計的思路，建立了飛航導彈渦扇發動機一體化設計的優化設計模型並給出了算例和分析。 -
The constrain - analyzed results and the mission - analyzed results of some maneuverable missiles indicate that the model of maneuverable missile and turbofan integrated constrain analysis and mission analysis is feasible and available
對飛航導彈的約束分析計算結果和任務分析計算結果表明，建立的飛航導彈渦扇發動機一體化約束分析與任務分析模型是合理可行的，具有很好的工程實用價值。 -
At the same time, h guidance law of the air - air missile is designed with l2 gain theory and the h2 / hx mixed control theory to minish the sensitivity to maneuverable goal
同時基於不確定非線性系統的幾增益理論和h : / hao混合控制理論研究了空一空導彈的h 』魯棒制導律的設計，以減小空一空導彈制導律對目標機動的敏感性。
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