三单元体旋转型惯导系统数据采集关键技术研究
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北京航空航天大学,北京航空航天大学,北京航空航天大学,北京航空航天大学

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985工程


Research on the key technology of data acquisition for tri-unit rotating inertial navigation system
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Beijing University of Aeronautics and Astronautics,Beijing University of Aeronautics and Astronautics,Beijing University of Aeronautics and Astronautics,Beijing University of Aeronautics and Astronautics

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985project

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    摘要:

    三单元体旋转型捷联惯导系统相对传统捷联惯导系统和现有的其它旋转型惯导系统都具有诸多优势,但对其数据采集环节也提出了一些新问题。针对系统数据采集量大、同步性要求高等特点,详细分析了惯性器件之间、惯性器件与光栅之间数据采集时间不同步的影响,提出了相应解决方案;针对温度采集易受电机旋转影响的现象,具体阐述了造成影响的原因,采取了相应措施,并从硬件上设计了一种数字式温度传感器DS18b20与DSP通讯的新模式。测试结果表明,数据采集单元达到了预期设计指标,为高精度低成本惯导系统的实现建立了基础。

    Abstract:

    Compared with the classical strap-down inertial navigation system and the rotating inertial navigation system in being, tri-unit rotating strap-down inertial navigation system has many advantages. Nevertheless, it brings some new problems to data acquisition. In view of the characteristic of this system, such as large amount of data, strong requirement on time synchronization, the impact of time asynchronization both between inertial sensors and between inertial sensors and gratings was analyzed in detail. At the same time, the corresponding solution project was given. In view of the phenomenon that temperature acquisition was disturbed by the rotation of motor easily, the causes were described concretely and relevant measures were taken as well. What’s more, a new communication between digital temperature sensor DS18B20 and DSP was designed in hardware. The result shows the data acquisition instrument comforts anticipative requirements and lay a good foundation for the coming out of high-precision, low-cost inertial navigation system.

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王蕾,陈松,徐烨烽,慈海波.三单元体旋转型惯导系统数据采集关键技术研究[J].数据采集与处理,2013,28(1):

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  • 收稿日期:2011-09-18
  • 最后修改日期:2011-11-29
  • 录用日期:2011-12-26
  • 在线发布日期: 2013-05-27