首页 | 本学科首页   官方微博 | 高级检索  
     

基于数字仿真的再入飞行器滚转异常边界条件研究
引用本文:南英 陈士橹. 基于数字仿真的再入飞行器滚转异常边界条件研究[J]. 宇航学报, 1997, 18(1): 18-22
作者姓名:南英 陈士橹
作者单位:北京航空航天大学,西北工业大学
摘    要:提出了一种基于数字仿真的再入弹头滚转异常边界条件的确定方法。即:首先给出可精确描述考虑各种气动力(矩)系数、各种干扰源作用时的六自由度运动方程。针对各种干扰源及其组合作用,对某弹头的滚转异常现象作了大量的数字仿真。文中采用一种拟合方法,妥善处理了这些仿真结果,拟合出该弹头滚转异常边界条件的近似解析式

关 键 词:再入飞行器  滚转异常  边界条件

UNUSUAL ROLLING BOUNDARY CONDITION OF REENTRY VELICLES BASED ON NUMERICAL SIMULATION
Nan Ying. UNUSUAL ROLLING BOUNDARY CONDITION OF REENTRY VELICLES BASED ON NUMERICAL SIMULATION[J]. Journal of Astronautics, 1997, 18(1): 18-22
Authors:Nan Ying
Affiliation:Nan Ying (Beijing University of Aeronautics and Astronautics) Chen Shilu Yan Hui (Northwestern Polytechnical University)
Abstract:A monthed is presented to determine the unusual rolling boundary condition of a reentry vehicle based on the numerical simulation A six freedom equations of motion are given to exactly consider many kinds of disturbances and all kinds of aerodynamic coefficients A lot of numerical simulations have been done for the unusual rolling of a reentry vehicle considering the disturbances The paper stadied a numerical method to deal with the large amount numerical results and obtained an approximate analytical formula to calculate the unusual rolling boundary condition of the reentry vehicle
Keywords:Reentry vehicle Unusual rolling Boundary condition
本文献已被 CNKI 维普 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号