An Analysis Of The Maximum Time Rates of Heat of Long-Range Boost Glide Flight;
助推-远程滑翔三维飞行的热流峰值分析
The trajectory was divided into boost phase and glide phase,which were optimized respectively and the optimal trajectory was obtained.
将再入航迹分为助推加速段和无动力滑翔段分别优化,从而得到优化航迹。
Attribute reduction-based boosting and its application;
基于属性约减的助推技术及其应用
The boosting technology is important to improve the penetration ability of the earth penetrating weapon(EPW).
应用助推技术是提高钻地弹侵彻能力的重要手段。
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