| 导弹姿态控制系统最佳测试点的选取 |
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| 引用本文： | 王建宏,许化龙,曹祥宇.导弹姿态控制系统最佳测试点的选取[J].上海航天,2003,20(1):50-52. |
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| 作者姓名： | 王建宏 许化龙 曹祥宇 |
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| 作者单位： | 西安第二炮兵工程学院,陕西,西安,710025 |
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| 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，达到了以最小测试点和最短时间来检测与隔离故障的目的
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| 关 键 词： | 导弹 姿态控制系统 测试点 选取 故障检测 |
| 文章编号： | 1006-1630(2003)01-0050-03 |
| 修稿时间： | 2002年9月20日 |
Determination of the Optimal Testing Points for Missile Attitude Control System |
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| WANG Jian hong,XU Hua long,CAO Xiang yu.Determination of the Optimal Testing Points for Missile Attitude Control System[J].Aerospace Shanghai,2003,20(1):50-52. |
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| Authors: | WANG Jian hong XU Hua long CAO Xiang yu |
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| Abstract: | 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. |
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| Keywords: | Optimal testing points Missile Attitude control system Fault detection |
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