基于联邦卡尔曼滤波的GPS辅助惯性导航系统的研制

International Conference on Recent Advances in Space Technologies, 2003. RAST '03. Proceedings of Pub Date : 1900-01-01 DOI:10.1109/RAST.2003.1303978

C. Hajiyev, M. A. Tutucu

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引用次数: 5

摘要

本文提出了一种GPS辅助惯性导航系统的算法。为此，设计了联邦卡尔曼滤波器，它包括两种不同的卡尔曼滤波器，并实时处理INS和GPS数据。仿真结果表明，利用GPS辅助惯导系统对运动参数的估计精度较高。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Development of GPS aided INS via Federated Kalman filter

In the paper an algorithm on aiding the Inertial Navigation System with GPS is presented. Federated Kalman filter, which includes two different Kalman filters and processes INS and GPS data in real time, is designed for this reason. Simulation is made and presented on the flight dynamics, and it is determined that the algorithm for aiding the INS with GPS, evaluates the motion parameters with high accuracy.

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International Conference on Recent Advances in Space Technologies, 2003. RAST '03. Proceedings of

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