液体推进剂导弹全动力系统动态故障仿真(二)  

Simulation of Steady-state Fault for Whole Liquid Propellant Missile Power System

作　　者：张炜[1] 徐志高[1] 黄先祥[1] 

机构地区：[1]第二炮兵工程学院,西安710025

出　　处：《系统仿真学报》2004年第6期1178-1180,共3页Journal of System Simulation

摘　　要：为了分析其故障特性和获取各种动态故障模式,采用性能优良的Runge-Kutta-Fehlberg(R-K-F)方法求解动态故障模型方程,仿真液体推进剂导弹(液体导弹)动力系统全系统动态故障。对已发生过或可能出现的故障形式,进行了过渡过程动态故障模拟计算和特性分析,获得了动力系统全系统动态故障模式库。计算结果表明,所建模型正确合理,数值模拟计算方法满足要求。该研究开辟了导弹动力系统动态过程故障分析、检测和诊断方法的新途径。In order to analyze dynamic fault characteristic and to acquire all dynamic fault patterns, the Runge- Kutta- Fehlberg (R-K-F) method is employed to solve equations of dynamic model for the whole missile power system. The dynamic fault simulating computation and characteristic analysis of transition process is performed under fault conditions, so the dynamic fault pattern base for whole power system is acquired. The calculated results show that the established model is reasonable and the numerical simulation method is effective. The study pioneers the way of fault analysis, detection and diagnosis method for dynamic process of whole liquid missile power system.

关 键 词：液体推进剂导弹 动力系统 故障模拟 故障特性分析 模式获取 

分 类 号：TP182[自动化与计算机技术—控制理论与控制工程]