上海航天（中英文）2024，Vol.41Issue(3)：110-120,11.DOI:10.19328/j.cnki.2096-8655.2024.03.012
助推滑翔变体飞行器弹道方案多目标近似优化
Multi-objective Approximate Optimization for the Boost-glide Morphing Flight Vehicle Trajectory Scheme
摘要
Abstract
Aiming at the problems such as the difficulty in optimizing morphing and the contradiction of multiple design objectives,the multi-objective approximate optimization for the boost-glide morphing flight vehicle trajectory scheme is studied.First,the optimization framework of an all-course trajectory scheme for boost-glide morphing flight vehicles is proposed,and the control parameters and trajectory scheme parameters are optimized through the inner and outer layers,respectively.Then,a multi-objective optimization model is formulated for the trajectory scheme that optimizes a target with the minimum takeoff mass and the maximum flight range.In the trajectory modeling,the boost stage trajectory model is constructed based on the Newton iteration method,and the optimal morphing model of reentry glide stage trajectory is established based on the pseudo-spectral method.Furthermore,a multi-objective approximate constrained optimization method based on differential evolution(MACO-DE)is proposed to optimize the boost-glide morphing flight vehicle trajectory scheme.Compared with the initial scheme,the take-off mass can be reduced by 3.81%at the same flight range,and the flight range can be improved by 6.62%at the same take-off mass,which demonstrates the reasonability of the all-course trajectory scheme and the effectiveness of the MACO-DE.关键词
助推滑翔变体飞行器/全程弹道/弹道优化/多目标优化/近似优化Key words
boost-glide morphing flight vehicle/all-course trajectory/trajectory optimization/multi-objective optimization/approximate optimization分类
航空航天引用本文复制引用
翟艺云,龙腾,刘震宇,史人赫,叶年辉..助推滑翔变体飞行器弹道方案多目标近似优化[J].上海航天（中英文）,2024,41(3):110-120,11.基金项目
国家自然科学基金(52272360,52005288,52232014) （52272360,52005288,52232014）
北京市自然科学基金(3222019) （3222019）
