现代防御技术2011，Vol.39Issue(4)：15-18,25,5.DOI:10.3969/j.issn.1009-086x.2011.04.004
远程火箭弹滑翔增程技术研究
Research on Gliding Extended Range in Long Rang Rocket Missile
杨泗智 1胡宽荣1
作者信息
- 1. 西安东方集团有限公司,陕西西安710043
- 折叠
摘要
Abstract
Based on the rocket projectile with gliding extended range, making use of the method of controlling the normal acceleration and holding on the ratio of the lift force and the maximal drag force, the model of glider missile has been established, the constraint conditions of the two methods have been analyzed and the flight ballistic has been simulated, and furthermore, the influence on the ballistic trajectory of the different start point in flight path angle has been computed. The result shares reference value for selecting the control method in the design of gliding extended projectiles.关键词
火箭弹/飞行弹道/滑翔增程/弹道控制Key words
rocket projectile/ flight trajectory( ballistic) / gliding extended range/ trajectory control分类
军事科技引用本文复制引用
杨泗智,胡宽荣..远程火箭弹滑翔增程技术研究[J].现代防御技术,2011,39(4):15-18,25,5.
