| 捷联惯导系统计算机硬件检测原理与实现 |
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| 引用本文： | 赵勇,欧刚.捷联惯导系统计算机硬件检测原理与实现[J].北京航空航天大学学报,1991(1):49-53. |
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| 作者姓名： | 赵勇 欧刚 |
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| 作者单位： | 北京航空航天大学自动控制系
(赵勇，欧刚)，北京航空航天大学自动控制系(崔中兴) |
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| 摘 要： | 介绍一种实用捷联惯导系统计算机结构。主模块与美国SESCO/TITAN公司的SECS86/20模块兼容,检测软件可以检测板上大中规模集成芯片,具有检测全面、准确的特点,从方法与原理上都具有通用性,可以方便地移植到其它类似的机器上。该软件已用于实际系统。
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| 关 键 词： | 惯性导航系统 捷联式 计算机 检测 |
THE PRINCEPLES AND IMPLEMENT OF COMPUTERHAR DWARE TEST IN STRAPDOWN INERTIAL NAVIGATION SYSTEM |
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| Zhao Yong Ou Gang Cui Zhongxing.THE PRINCEPLES AND IMPLEMENT OF COMPUTERHAR DWARE TEST IN STRAPDOWN INERTIAL NAVIGATION SYSTEM[J].Journal of Beijing University of Aeronautics and Astronautics,1991(1):49-53. |
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| Authors: | Zhao Yong Ou Gang Cui Zhongxing |
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| Institution: | Dept. of Auto. Control |
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| Abstract: | A practical computer structure of Strapdown Inertial Navigation System is introduced. The main module board is compatible with SECS86/20 module board of SECCO/TITAN corporation. The test program can accurately verify large and middle scale integrated chips of the computer system. The software modules are transplantable and replaceable without the need for special tools. The test program has been used in the practical system. |
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| Keywords: | computer hardware test strapdown inertial navigation system computer system |
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