| 惯性／GPS组合导航系统飞行试验技术 |
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| 引用本文： | 王义珍,冀军胜. 惯性／GPS组合导航系统飞行试验技术[J]. 中国惯性技术学报, 1996, 0(3) |
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| 作者姓名： | 王义珍 冀军胜 |
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| 作者单位： | 中国飞行试验研究院哈尔滨工程大学４０２教研室 |
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| 摘 要： | —本文通过对差分ＧＰＳ动态定位精度的飞行验证及以差分ＧＰＳ为基准测定组合导航系统精度的科研试飞说明：目前采用差分ＧＰＳ来鉴定组合导航系统的位置、速度精度是满意的。本报告还论述对组合导航系统飞行试验技术的设想
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| 关 键 词： | 组合导航 飞行试验 |
Flight Test Technology of INS/GPS Integrated Navigation System |
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| Wang Yizhen Ji Junsheng. Flight Test Technology of INS/GPS Integrated Navigation System[J]. Journal of Chinese Inertial Technology, 1996, 0(3) |
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| Authors: | Wang Yizhen Ji Junsheng |
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| Affiliation: | Flight Test Research Institute of China |
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| Abstract: | This paper describes through the flight test demonstration of dynamic position accuracy of difference GPS: at present, to evaluate the position and velocity accuracy of the integrated navigation system with difference GPS is successful. And it also describes the planning study of the flight test technology of the integrated navigation system. |
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| Keywords: | integrated navigation flight test |
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