| 基于虚拟仪器的空中加油吊舱联调测控系统设计 |
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| 引用本文： | 苏新兵,胡良谋,曹克强,李小刚.基于虚拟仪器的空中加油吊舱联调测控系统设计[J].机床与液压,2012,40(3):99-102. |
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| 作者姓名： | 苏新兵 胡良谋 曹克强 李小刚 |
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| 作者单位： | 空军工程大学工程学院,陕西西安,710038 |
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| 基金项目： | 中国博士后科学基金资助项目，中国博士后科学基金特别资助项目 |
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| 摘 要： | 进行了基于虚拟仪器的空中加油吊舱联调系统设计,给出了测控系统的硬件组成,设计了各测试通道的数据采集方案和测试软件。试验结果证明:该测试系统具有效率高、误差小和自动化程度高等特点,具有良好的推广应用前景。
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| 关 键 词： | 虚拟仪器 空中加油吊舱 联调系统 |
Design on Combined Debugging Test System for Aerial Refueling Pod Based on Virtual Instrument Technology |
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| SU Xinbing
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HU Liangmou
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CAO Keqiang
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LI Xiaogang.Design on Combined Debugging Test System for Aerial Refueling Pod Based on Virtual Instrument Technology[J].Machine Tool & Hydraulics,2012,40(3):99-102. |
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| Authors: | SU Xinbing HU Liangmou CAO Keqiang LI Xiaogang |
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| Affiliation: | (The Engineering Institute,Air Force Engineering University,Xi’an Shaanxi 710038,China) |
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| Abstract: | Combined debugging test system for aerial refueling pod was design based on virtual instrument technology.The hardware composing of the system was presented.The data collection scheme and testing software for each testing channel were designed.The testing results testify that the system has advantages of high efficiency,diminutive error and high automatization.It has very good prospects for generalization. |
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| Keywords: | Virtual instrument technology Aerial refueling pod Combined debugging test system |
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