Optimal trajectory and heat load analysis of different shape lifting reentry vehicles for medium range application

查看全文 作　　者：S.Tauqeer ul Islam [1]RIZVI;Lin-shu [1]HE;Da-jun [1]XU

机构地区：[1]School of Astronautics,Beihang University

出　　处：《Defence Technology(防务技术)》索引2015年第11卷第4期,共12页

基　　金：the Chinese Scholarship Council for supporting the research 摘　　要：The objective of the paper is to compute the optimal burn-out conditions and control requirements that would result in maximum down-range/cross-range performance of a waverider type hypersonic boost-glide(HBG) vehicle within the medium and intermediate ranges,and compare its performance with the performances of wing-body and lifting-body vehicles vis-a-vis the g-load and the integrated heat load experienced by vehicles for the medium-sized launch vehicle under study.Trajectory optimization studies were carried out by considering the heat rate and dynamic pressure constraints.The trajectory optimization problem is modeled as a nonlinear,multiphase,constraint optimal control problem and is solved using a hp-adaptive pseudospectral method.Detail modeling aspects of mass,aerodynamics and aerothermodynamics for the launch and glide vehicles have been discussed.It was found that the optimal burn-out angles for waverider and wing-body configurations are approximately 5° and 14.8°,respectively,for maximum down-range performance under the constraint heat rate environment.The down-range and cross-range performance of HBG waverider configuration is nearly 1.3 and 2 times that of wing-body configuration respectively.The integrated heat load experienced by the HBG waverider was found to be approximately an order of magnitude higher than that of a lifting-body configuration and 5 times that of a wing-body configuration.The footprints and corresponding heat loads and control requirements for the three types of glide vehicles are discussed for the medium range launch vehicle under consideration. 关键词：再入飞行器载荷分析最佳轨迹翼身组合体形状最优控制问题控制要求运载火箭

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Optimal trajectory and heat load analysis of different shape lifting reentry vehicles for medium range application

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