高超声速变体飞行器优化设计的概念研究
onceptual research on optimization design for hypersonic morphing vehicle
针对高超声速变体飞行器优化设计问题进行研究,首先基于高超声速计算力学理论,采用反演一体化设计方法,建立高超声速变体飞行器模型,然后选取高超声速变体飞行器的模型参数,依据乘波飞行的特点,构造优化性能指标,进而采用变尺度法对性能指标函数进行迭代寻优,获取高超声速变体飞行器最佳的模型参数,最后通过仿真分析来验证方法的有效性。
his paper will research optimization design problems for hypersonic morphing vehicle. Firstly based on the theories of hypersonic computational mechanics, inversion design methods are applied to establish hypersonic morphing vehicle mode. Secondly by selecting hypersonic morphing vehicle model parameters, optimization performance indexes are structured according to wave-rider flight characteristics. Then variable metric algorithm is used to iteratively optimize performance index function, and optimum model parameters are obtained for hypersonic morphing vehicle. Lastly method effectiveness is verified by simulation analysis.
刘燕斌、姚克明、陆宇平、张侃
航空航天技术
高超声速飞行变体飞行器优化设计控制要求乘波特性
aerospace vehiclehypersonic flightwaveriderinversion designfeedback control
刘燕斌,姚克明,陆宇平,张侃.高超声速变体飞行器优化设计的概念研究[EB/OL].(2010-07-01)[2025-08-02].http://www.paper.edu.cn/releasepaper/content/201007-13.点此复制
评论