| 一种基于多模型的航天试验效果实时评估方法 |
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| 引用本文： | 朱祥玲,吴钦章,胡志宏. 一种基于多模型的航天试验效果实时评估方法[J]. 测控技术, 2015, 34(1): 153-156. DOI: 10.3969/j.issn.1000-8829.2015.01.042 |
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| 作者姓名： | 朱祥玲 吴钦章 胡志宏 |
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| 作者单位： | 1. 中国科学院光电技术研究所,四川成都610209;中国科学院大学,北京100049;中国人民解放军63796部队,四川西昌615000;2. 中国科学院光电技术研究所,四川成都,610209;3. 中国人民解放军63796部队,四川西昌,615000 |
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| 摘 要： | 依据遥测参数表征的航天器飞行状态物理含义及航天器工作部件技术状态,建立了多种分析评估模型,将航天试验效果的综合评估转换为多个关键动作、系统主要部件及具体测量参数正常与否的判断,实现了航天试验效果快速、准确、全面的评估.经仿真验证,评估方法准确可行,可在5 min内完成航天试验效果评估.
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| 关 键 词： | 遥测参数 航天器 飞行试验 实时评估 |
A Real-time Assessment Method for Space Testing Based on Multimodels |
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| ZHU Xiang-ling , WU Qin-zhang , HU Zhi-hong. A Real-time Assessment Method for Space Testing Based on Multimodels[J]. Measurement & Control Technology, 2015, 34(1): 153-156. DOI: 10.3969/j.issn.1000-8829.2015.01.042 |
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| Authors: | ZHU Xiang-ling WU Qin-zhang HU Zhi-hong |
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| Abstract: | Based on the analysis of correlation between telemetry parameter,including the characterization,the flight state,the physical meaning and the main technology components of the spacecraft,some evaluation models are proposed,which can realize the comprehensive assessment of aerospace launching by judging the key actions,the main components of the launch vehicle and specific measurement parameters.With the comprehensive utilization of the telemetry information,the accurate assessment can be provided within 5 min. |
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| Keywords: | telemetry parameters launch vehicle flight test real time evaluation |
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