Six-Degree-Freedom Full-Quantity Mathematical Modeling and Simulation of Launch Vehicle Control System

摘要：

This paper selects a type of launch vehicle as research background and its control system as research object. The six-degree-freedom full-quantity mathematical modeling and simulation method of the flying launch vehicle have been fully discussed in the paper. The technology brought forward in this paper utilizes comparative integrated and accurate mathematical models and analyzes simulation results of different interferences, thus greatly increases the reliability and precision of simulation. It can be taken as a valuable reference to other integrative simulations of complex systems.

关键词： control system six-degree-freedom mathematical modeling simulation

作者: YANG Ping SUN Gang CI Ying

作者单位: The Academy of Equipment Command &Technology,Beijing 101416,China;Beijing Institute of Tracing and T Beijing Institute of Tracing and Telecommunication Technology, Beijing 100094,China

会议类型: 国际会议

会议名称: 第七届国际测试技术研讨会

会议地点: 北京

会议语种:英文

在线出版日期: 2007-08-05（万方平台首次上网日期，不代表论文的发表时间）