| 一种统一惯性导航方法 |
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| 引用本文： | 魏宗康,黄云龙.一种统一惯性导航方法[J].导航与控制,2017(6):1-4. |
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| 作者姓名： | 魏宗康 黄云龙 |
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| 作者单位： | 北京航天控制仪器研究所,北京,100039 |
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| 基金项目： | 国防科技创新特区(编号:17-0163-15-XJ-002-002-10) |
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| 摘 要： | 捷联式和平台式惯性导航系统的导航方程不同:同一惯性测量系统选取不同导航坐标系时,导航方程也不同;各类力学编排形式多样、结构复杂且输出结果具有局限性.针对这些问题,提出一种统一惯性导航方法.惯性导航试验结果表明,基于统一惯性导航方程与基于传统惯性导航方程解算的结果一致,验证了统一惯性导航方程的有效性.
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| 关 键 词： | 惯性导航 导航方程 平台惯性导航 捷联惯性导航 |
A Kind of Unified Inertial Navigation Method |
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| WEI Zong-kang and HUANG Yun-long.A Kind of Unified Inertial Navigation Method[J].Navigation and Control,2017(6):1-4. |
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| Authors: | WEI Zong-kang and HUANG Yun-long |
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| Institution: | Beijing Institute of Aerospace Control Devices, Beijing 100039 and Beijing Institute of Aerospace Control Devices, Beijing 100039 |
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| Abstract: | Aiming at the problem that strapdown inertial navigation system (SINS) and platform inertial navigation system (PINS) have different navigation equations:an inertial measurement system would also have different navigation e-quations while choosing a variety of navigation coordinates, mechanical arrangements have different forms, complicated structures and limited output, a kind of unified inertial navigation method was put forward. The results of the inertial navi-gation test show that the results based on the unified inertial navigation equation are consistent with those calculated by tra-ditional inertial navigation equations, and the validity of the unified inertial navigation equation is verified. |
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| Keywords: | inertial navigation navigation equation platform inertial navigation system strapdown inertial navigation system |
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