| 飞航导弹总体参数优化设计研究 |
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| 引用本文： | 杨国平. 飞航导弹总体参数优化设计研究[J]. 战术导弹技术, 2000, 0(3) |
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| 作者姓名： | 杨国平 |
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| 作者单位： | 洪都航空工业集团!南昌330024 |
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| 摘 要： | 以空气喷气型飞航导弹为研究对象 ,探讨其主要总体参数优化设计效果 .通过建立全弹质量计算模型、气动估算模型和涡喷发动机性能插算等数学模型 ,选取一定的控制规律进行了质点弹道计算 .在满足总体战术技术指标前提下 ,以航程最远作为目标函数 ,对导弹 5个总体参数进行了优化设计 ,所得结果令人满意
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| 关 键 词： | 飞航导弹 总体设计 参数优化 参数分析 数学模型 |
Research on the Configuration Parameter Optimization of Cruise Missile |
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| YANG Guo ping. Research on the Configuration Parameter Optimization of Cruise Missile[J]. Tactical Missile Technology, 2000, 0(3) |
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| Authors: | YANG Guo ping |
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| Abstract: | Thc effect of the main configuration parameters optimization design of the cruise missile is discussed,with the air jet cruise missile as the study subject.The particle trajectory is calculated with certain amoune of selected control rules by establishing mathematical mod els such as whole missile mass calculation model,aerodynamic estimation model and turbojet engine performance interpolation.On the premise of meeting the total tactical indices ,taking the longest range as the target function,five configuration parameters of the missile have been designed optimistically,the result of which is satisfactory. |
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| Keywords: | cruise missile configuration design parameter optimization parametric analysis mathematical model |
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