国防科技大学学报2017，Vol.39Issue(4)：56-61,6.DOI:10.11887/j.cn.201704009
机动发射条件下助推滑翔导弹射击诸元快速解算
Efficient method for firing data calculation of boost-glide missile in mobile condition
摘要
Abstract
Considering the urgent need of rapid trajectory generation of boost-glide missile in mobile condition, seven key parameters of control variables were selected as the firing data, and the corresponding iterative calculation algorithms were proposed.The full-range trajectory was divided into the boost phase, initial phase, glide phase and dive attack phase, all these flight phases were described in a unified dynamics model.Firing data in different phases were calculated rapidly one by one, and multiple constraints were satisfied strictly, with the help of the parameterized iterative algorithm.Furthermore, a partly recalculation mode which uses the firing data of the center trajectory in the boost phase and recalculates the others was proposed on the basis of the full mode.The simulation results indicate that this method can achieve a great performance in the quick attack to a ground stationary target in mobile condition.关键词
助推滑翔导弹/机动发射/全程弹道/诸元解算Key words
boost-glide missile/mobile launch/full-range trajectory/calculation of firing data分类
航空航天引用本文复制引用
何睿智,刘鲁华,汤国建,包为民..机动发射条件下助推滑翔导弹射击诸元快速解算[J].国防科技大学学报,2017,39(4):56-61,6.基金项目
国家自然科学基金资助项目(11502289) （11502289）
