导弹姿态控制系统最佳测试点的选取  

Determination of the Optimal Testing Points for Missile Attitude Control System

作　　者：王建宏[1] 许化龙[1] 曹祥宇[1] 

机构地区：[1]西安第二炮兵工程学院,陕西西安710025

出　　处：《上海航天》2003年第1期50-52,共3页Aerospace Shanghai

摘　　要：以导弹姿态控制系统框图和信号流程为基础 ,确定了故障信息矩阵 ,通过分析测试点的加权值 ,用逐步分解矩阵的方法选出最佳测试点 ,确定最佳诊断步骤 。The matrix of fault information is structured based on functional block diagram and signal flow of the missile attitude control system. Optimal testing points are selected by analyzing its weight and decomposing the matrix, so that the optimal diagnostic procedure is determined and the object to isolate the faults of missile attitude control system with the least testing points and the shortest time is fulfilled.

关 键 词：导弹 姿态控制系统 测试点 选取 故障检测 

分 类 号：TJ765.23[兵器科学与技术—武器系统与运用工程] TJ765.41