| 长征六号运载火箭动力测发控系统仿真测试平台的设计 |
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| 引用本文： | 马玉璘,陈文浩,刘伟,袁企乡,蔡珂.长征六号运载火箭动力测发控系统仿真测试平台的设计[J].应用声学,2017,25(5):1-3. |
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| 作者姓名： | 马玉璘 陈文浩 刘伟 袁企乡 蔡珂 |
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| 作者单位： | 上海航天电子技术研究所,上海 201109,上海航天电子技术研究所,上海 201109,上海航天电子技术研究所,上海 201109,上海航天电子技术研究所,上海 201109,上海航天电子技术研究所,上海 201109 |
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| 摘 要： | 针对长征六号运载火箭动力测发控系统射前仿真测试需求,结合短周期快速发射及方舱操作的特点,设计了一种仿真测试平台；该测试平台使用电气信号模拟动力配气台阀门、压力传感器及箭体连接器硬件接口信号,形成硬件接口层；采用软件模拟配气台工作原理,仿真箭体连接器通断,并模拟基地加注间通讯系统与动力测发控系统进行信息交互,形成软件模型层；硬件接口层与软件模型层之间通过RS422总线和PC104总线连接,实现仿真测试平台的模块化和组合化设计；该仿真测试平台为长征六号运载火箭动力测发控系统提供了闭环测试环境；实际情况表明,该仿真测试平台可覆盖动力测发控系统的全部工作状态,满足短周期快速发射的测试需求,提高了动力测发控系统仿真测试的效率。
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| 关 键 词： | 长征六号 动力测发控 仿真测试 |
| 收稿时间： | 2017/3/9 0:00:00 |
| 修稿时间： | 2017/3/24 0:00:00 |
Design of Power Control and Testing Simulation System for CZ-6 Rocket |
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| Ma Yulin,Chen Wenhao,Liu Wei,Yuan Qixiang and Cai Ke.Design of Power Control and Testing Simulation System for CZ-6 Rocket[J].Applied Acoustics,2017,25(5):1-3. |
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| Authors: | Ma Yulin Chen Wenhao Liu Wei Yuan Qixiang and Cai Ke |
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| Institution: | Shanghai Aerospace Electronic Technology Institute,Shanghai 201109,China,Shanghai Aerospace Electronic Technology Institute,Shanghai 201109,China,Shanghai Aerospace Electronic Technology Institute,Shanghai 201109,China,Shanghai Aerospace Electronic Technology Institute,Shanghai 201109,China and Shanghai Aerospace Electronic Technology Institute,Shanghai 201109,China |
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| Abstract: | A simulation platform of power control and testing system for CZ-6 rocket was designed in this paper.The requirement,the framework and software of the platform were introduced. The platform simulate power system units in order to compose a integrated test envirment with power control and testing system.The experiment showed the platform tested all work status of power system and the requirement was met.. |
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