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GPS/IRS伪距组合技术研究 被引量:2

Research on GPS/IRS Pseudo-range Integration Technology
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摘要 一本文结合一典型的反舰战术导弹的中程制导任务,对GPS/IRS伪距组合系统进行了分析和研究.采用U-D分解卡尔曼滤波对组合系统进行了Monte-Carlo仿真。结果表明,GPS/IRS组合作为提高导航、制导精度的有效途径,可以克服纯惯性系统中存在的无界位置误差。不同的陀螺精度的仿真还表明,组合系统对一定范围内的陀螺精度的降低不敏感。(这为在进行GPS/中等精度、低成本的航姿系统组合时降低对陀螺的精度要求提供了理论依据) his paper analyzes and studies a navigation system by using GPS/IRS(Inertial Reference System) integration technology based on the program of developing a guidance device for a typical anti-ship tactical missile. The U-D decomposed Kalman filter is used in the Monte-Carlo simulation for this integrated system. The result shows that GPS/IRS integration technique is an effective way for improving the accuracy of navigation and guidance system,and will eliminate the boundless position er-rors that exit in all pure IRSS.The simulations for integrated system by using different gyro drifts lead to the conclusion that a system like this one is not sensitive to the reduce of the gyro's accuracy within a certain range.(This provides a theoretical founda-tion for the development of integrated system by combining GPS with a low-cost heading & attitude system and can reduce the influence due to the lower-down of the gyro's accuracy.)
出处 《中国惯性技术学报》 EI CSCD 1995年第4期9-14,共6页 Journal of Chinese Inertial Technology
关键词 卡尔曼滤波器 U-D因子分解 伪距 GPS IRS Kalman filter U-D factor decomposition pseudo-range GPS IRS
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参考文献1

  • 1王壬林.惯性加速度计与气压高度计之随机误差模型的辨识与估计[J]航空学报,1985(06).

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