| 一种火箭主动段弹道数据融合方法 |
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| 引用本文： | 杨鼎新,杜鹏.一种火箭主动段弹道数据融合方法[J].自动化技术与应用,2014,33(12):14-16. |
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| 作者姓名： | 杨鼎新 杜鹏 |
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| 作者单位： | 中国卫星海上测控部,江苏江阴,214431 |
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| 摘 要： | 提出了一种火箭主动段弹道数据融合方法,该方法利用各类测量弹道数据进行融合计算,得出一组综合弹道数据为测量设备提供数字引导,并作为判断火箭飞行轨迹的依据。通过以往某次火箭主动段任务实测数据复演,验证了这种方法的可行性和有效性。
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| 关 键 词： | 弹道 数据融合 支持度 |
A Fusion Arithmetic for Trajectory Data in Rocket Powered Phase |
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| YANG Ding-xin,DU Peng.A Fusion Arithmetic for Trajectory Data in Rocket Powered Phase[J].Techniques of Automation and Applications,2014,33(12):14-16. |
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| Authors: | YANG Ding-xin DU Peng |
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| Affiliation: | (China Satellite Measure and Track Centre Jiangyin 214431 China ) |
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| Abstract: | This paper proposes a fusion arithmetic for trajectory data in rocket powered phase. The method uses a variety of trajectory data, it can get for fusion calculation, then can educe a compositive trajectory data for digital-guided, and regards as the basis of judging the rocket flight state. Through the active phase of the rocket task data playback, to verify the practicability and effectiveness. |
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| Keywords: | trajectory data fusion degree of support |
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