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鸭式制导炮弹气动布局参数设计方法研究

Investigation of Aerodynamic Configuration Design Method for Canard Guided Projectile

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【作者】 常思江王中原魏伟卫东华

【Author】 CHANG Sijiang1,WANG Zhongyuan1,WEI Wei1,WEI Donghua2(1 School of Power Engineering,NUST,Nanjing 210094,China;2 Nanjing Center,Heilongjiang North Tools Co.Ltd,Nanjing 210094,China)

【机构】 南京理工大学动力工程学院黑龙江北方工具有限公司南京中心

【摘要】 针对一对鸭舵的制导炮弹,提出采用模糊综合评判方法进行气动布局参数设计。选用一套气动力快速估算方法计算了制导炮弹的气动特性,分析了气动布局参数对气动特性的影响;建立了有控弹道模型,并在一定控制模式下对有控弹道特性进行了分析;综合考虑有控弹道设计的各项指标,应用模糊综合评判模型对气动布局参数进行了合理设计。算例结果表明,该设计方法具有良好的实用性和通用性。

【Abstract】 Focused on the guided projectile equipped with a canard,the fuzzy comprehensive evaluation method(FCEM) was proposed to design the aerodynamic configuration parameters.The aerodynamic characteristic of guided projectile was calculated by a set of aerodynamic fast algorithm.The influence of parameters on the aerodynamic characteristic was analyzed.The controllable trajectory model was established.The controllable trajectory characteristic was studied under a certain control mode.Considering several factors,the design of aerodynamic configuration parameters was done by using FCEM.Example results show that this method has practicability and generality.

  • 【文献出处】 弹箭与制导学报 ,Journal of Projectiles,Rockets,Missiles and Guidance , 编辑部邮箱 ,2009年05期
  • 【分类号】TJ011
  • 【被引频次】1
  • 【下载频次】266
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