摘要
本文研究了再入飞行器的优化气动布局问题，提出了单目标和多目标、优化设计方法。通过研究分析，指出了具有高机动性能的带翼机动再入飞行器、弯体机动再入飞行器及带翼锥柱裙机动再入飞行器等再入飞行器的几何参数变化规律。该研究对这类再入飞行器的气动布局选型有重要的参考价值。
Optimum aerodynamic configuration of reentry vehicle were studied.Single and mutiple objectives optimization methods were presented.The variations of geometry maneuvering reentry vehicle, were discussied while the characteristics of high able ability be provided.These studies are of important reference values to the designs of aerodynamic configuration of reentry vehicle.
出处
《宇航学报》
EI
CSCD
北大核心
1994年第3期64-70,共7页
Journal of Astronautics
关键词
多目标优化
气动布局
再入飞行器
Mutiple objectives optimization Aerodynamic configuration Reentry vehicle
