现代防御技术2011，Vol.39Issue(6)：111-116,6.DOI:10.3969/j.issn.1009-086x.2011.06.021
反解法在再入机动弹道设计中的应用研究
Application Research on Inverse Calculation Method for Reentry Maneuverable Trajectory
方喜龙 1刘新学 1梁建波 1王芳1
作者信息
- 1. 第二炮兵工程大学603教研室,陕西西安710025
- 折叠
摘要
Abstract
A general method of reentry maneuverable trajectory design is analyzed briefly. As the general method depended heavily on mathematical model and is sensitive for initial value, an inverse calculation method is presented. The method is based on the improved plane ballistic model and adopts the idea of error compensation. By calculating the trajectory inversely, the computational error of end point is moved to maneuvering point. Then the error can be compensated by adjusting the parameter of shutdown point or mid-course guidance. The result of simulation shows that the method is easy, feasible and effective.关键词
反解法/机动弹道/误差补偿/命中精度Key words
inverse calculation method/ maneuverable trajectory/ error compensation/ hit accuracy分类
军事科技引用本文复制引用
方喜龙,刘新学,梁建波,王芳..反解法在再入机动弹道设计中的应用研究[J].现代防御技术,2011,39(6):111-116,6.
