首页 | 本学科首页   官方微博 | 高级检索  
     


Hyper Heuristic Approach for Design and Optimization of Satellite Launch Vehicle
Authors:Amer Farhan RAFIQUEa  HE Linshua  Ali KAMRANb  Qasim ZEESHANa a
Affiliation:Amer Farhan RAFIQUEa,HE Linshua,Ali KAMRANb,Qasim ZEESHANa aDepartment of Spacecraft Technology,School of Astronautics,Beihang University,Beijing 100191,China bDepartment of Space Propulsion,China
Abstract:Satellite launch vehicle lies at the cross-road of multiple challenging technologies and its design and optimization present a typical example of multidisciplinary design and optimization(MDO) process.The complexity of problem demands highly effi-cient and effective algorithm that can optimize the design.Hyper heuristic approach(HHA) based on meta-heuristics is applied to the optimization of air launched satellite launch vehicle(ASLV).A non-learning random function(NLRF) is proposed to con-trol low-level me...
Keywords:multidisciplinary design optimization  satellite launch vehicle  heuristic optimization methods  hyper heuristic  air launched vehicles  
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《中国航空学报》浏览原始摘要信息
点击此处可从《中国航空学报》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号