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| 动基座对准试验及结果分析 | |
| 引用本文： | 胡国辉 王强. 动基座对准试验及结果分析[J]. 宇航学报, 1997, 18(3): 71-74 |
| 作者姓名： | 胡国辉 王强 |
| 作者单位： | 南京航空航天大学３０４教研室，哈尔滨工业大学控制工程系 |
| 摘 要： | 本文讨论了动基座对准的摇摆试验，设计了改进Ｋａｌｍａｎ滤波器，给出了试验结果和分析，得到了一些有益的结论。试验结果表明，该摇摆方案能满足某型号导弹的方位对准要求，只要将离线Ｋａｌｍａｎ滤波算法改为在线计算，即可进行方位的实时对准 |
| 关 键 词： | 动基座对准 摇摆试验 方位对准 |
EXPERIMENT OF TRANSFER ALIGNMENT AND ANALYSIS OF ITS RESULT |
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| Hu Guohui. EXPERIMENT OF TRANSFER ALIGNMENT AND ANALYSIS OF ITS RESULT[J]. Journal of Astronautics, 1997, 18(3): 71-74 | |
| Authors: | Hu Guohui |
| Abstract: | The vibration experiment of transfer alignment is studied in the paper We design improved Kalman filter,and analysis the experiment result to draw some good conclusion The result shows that the vibration method can satisfy azimuth alignment of the type of missile If off line Kalman filter is changed with on line Kalman filter,the real time alignment can be achieved |
| Keywords: | Transfer alignment Vibration experiment Arimuth alignment |
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