| LTN-72惯导设备在空间遥感器航空校飞中的应用 |
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| 引用本文： | 胡行毅,李保和.LTN-72惯导设备在空间遥感器航空校飞中的应用[J].遥感技术与应用,1993,8(3):26-31. |
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| 作者姓名： | 胡行毅 李保和 |
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| 作者单位： | 中国科学院空间科学与应用研究中心 100080 |
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| 摘 要： | 介绍了一种用于空间遥感器航空校飞的LTN-72惯导参数采集与传输装置。该装置能模拟星上数据管理系统(OBDH)传递包括校飞时间和全部LTN-72惯导参数在内的辅助数据,并具有输出检测信号和自检显示功能。装置经实际校飞使用,效果良好。
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| 关 键 词： | 遥感 惯导 微机 |
Application of LTN-72 Inertial Navigation System to the Flight Experiment for the Calibration of a Satellite-borne Remote Sensor |
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| Hu Xingyi Li Baohe Wang Jiaqi.Application of LTN-72 Inertial Navigation System to the Flight Experiment for the Calibration of a Satellite-borne Remote Sensor[J].Remote Sensing Technology and Application,1993,8(3):26-31. |
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| Authors: | Hu Xingyi Li Baohe Wang Jiaqi |
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| Affiliation: | (Centre for Space & Applied Research, Academia Sinica; 100080) |
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| Abstract: | This paper presents a navigational data acquicition and transmission device of LTN &;mdash; 72 inertial navigation equipment, which has been used in the flight experiment for the calibration of a satellite&;mdash;borne remote sensor. The result shows that both data and device are reliable. |
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| Keywords: | Remote sensing Inertial navigation Microcomputer |
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