| 一种动基座下ESGM定位误差仿真方法研究 |
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| 引用本文： | 潘弘涛,戴建国,屈炳辰.一种动基座下ESGM定位误差仿真方法研究[J].导航与控制,2015(3):103-107. |
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| 作者姓名： | 潘弘涛 戴建国 屈炳辰 |
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| 作者单位： | 海军潜艇学院;海军92330部队;海军潜艇学院 |
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| 摘 要： | 结合静电陀螺监控器的工作原理及天文导航知识，推导出ESGM 模型中导
航参数随载体运动而变化的计算方法，并用该方法仿真比较了各航行状态下ESGM 的定
位误差。结果表明：转向时的定位误差受航速、转向率的影响较大。该方法对动基座条
件下静电陀螺监控器的计算机仿真有一定参考价值。
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| 关 键 词： | 静电陀螺监控器 动基座 仿真 |
Reseach on Position Error of ESGM Simulation on Moving Base |
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| PAN Hong-tao,DAI Jian-guo and QU Bing-chen.Reseach on Position Error of ESGM Simulation on Moving Base[J].Navigation and Control,2015(3):103-107. |
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| Authors: | PAN Hong-tao DAI Jian-guo and QU Bing-chen |
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| Institution: | Navy Submarine Academy;Navy Army of 92330;Navy Submarine Academy |
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| Abstract: | Based on the principles of Electrostatic Supported Gyro Monitor(ESGM) and celestial navigation, we propose
a method to calculate the navigation parameters of ESGM for simulating, which changes with carrier moving. Using
this method we simulate and compare the error in different navigation. The test results show that: the steering error is influenced
by the speed and rate of steering. This method has a certain significance for the research of ESGM on moving base. |
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