南京理工大学学报（自然科学版）2011，Vol.35Issue(5)：610-613,620,5.
制导炮弹滑翔弹道优化设计方法研究
Optimization Design Method for Glide Trajectory of Guided Projectiles
摘要
Abstract
In order to obtain the optimal glide trajectory for the glide range-extended guided projectile (GREGP),the optimization glide flight kinematic equations in the vertical plane are established using Pontryagin minimum principle. The solution of the optimization glide trajectory is studied. The optimal control coefficients for glide flight of the GREGP are designed. The results show that the optimal lift coefficient can ensure the maximum range for the GREGP. The optimal lift coefficient changes near 1 and tends to be 1 finally.关键词
制导炮弹/滑翔弹道/优化设计Key words
guided projectiles/glide trajectory/optimation design分类
军事科技引用本文复制引用
史金光,王中原,孙洪辉,竹建东..制导炮弹滑翔弹道优化设计方法研究[J].南京理工大学学报（自然科学版）,2011,35(5):610-613,620,5.基金项目
江苏省"青蓝工程"资助项目 （）
南京理工大学科技发展基金(XKF09075) （XKF09075）
南京理工大学卓越计划"紫金之星"资助项目 （）
