| 某型飞行器全静压检测系统的设计实现 |
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| 引用本文： | 张劼,景博.某型飞行器全静压检测系统的设计实现[J].航空计算技术,2003,33(2):112-115. |
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| 作者姓名： | 张劼 景博 |
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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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| 摘 要： | 提出了以8031单片机为控制核心、基于振动筒式压力传感器的飞行器全静压自动检测系统的应用设计,论述了系统的构成和工作原理,对系统硬件电路和软件流程设计作了说明,给出了编程示例。系统设计的实现提高了飞行器全静压检测系统的自动化程度,具有检测速度快、精度高、判读直观,可靠性高和操作简单的特点,在实际测试中运行良好,性能稳定,具有良好的应用前景。
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| 关 键 词： | 飞行器全静压系统 单片机 自动测试系统 |
| 文章编号： | 1671-654X(2003)02-0112-04 |
| 修稿时间： | 2002年10月28 |
The Design and Realization of a Type Aerocraft Pitot-Static Pressure System |
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| ZHANG Jie,JING Bo.The Design and Realization of a Type Aerocraft Pitot-Static Pressure System[J].Aeronautical Computer Technique,2003,33(2):112-115. |
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| Authors: | ZHANG Jie JING Bo |
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| Abstract: | The design and realization way which bases on the 8031 microprocessor and vibrating pot pressure sensor in the aerocraft pitot-static pressure automatic measurement system is provided finally.the frame and work principles of the system are discussed in detail.Also,the hardware electric circuit and flow chart of software design are illuminated, a programme example is demonstrated. the system has characteristics of quick speed of testing, high precision, visual reading,high reliability and simple operation, and runs well and shows stable performance, so there is a broad and bright future waiting for it. |
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| Keywords: | aerocraft pitot-static pressure system single clip processor ATS |
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