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A Novel Initial Alignment Scheme for Low-Cost INS Aided by GPS for Land Vehicle Applications

机译:GPS辅助低成本低成本惯性导航系统初始对准方案

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This paper proposes a novel mechanism for the initial alignment of low-cost INS aided by GPS. For low-cost INS, the initial alignment is still a challenging issue because of the high noises from low-cost inertial sensors. In this paper, a two-stage Kalman Filtering mechanism is proposed for the initial alignment of low-cost INS. The first stage is designed for the coarse alignment. To solve the problems encountered by the general coarse alignment approach, an INS error dynamic accounting for unknown initial heading error is developed, and the corresponding observation equation, taking into account the unknown heading error, is also developed. The second stage is designed for the fine alignment, where the classical INS error dynamics based on small attitude error is used. Experimental results indicate that the proposed alignment approach can complete the initial alignment more quickly and more accurately compared with the conventional approach.
机译:本文提出了一种新型的GPS辅助低成本INS初始对准的机制。对于低成本INS,由于低成本惯性传感器产生的高噪声,初始对准仍然是一个具有挑战性的问题。本文提出了一种两阶段的卡尔曼滤波机制,用于低成本INS的初始对准。第一阶段设计用于粗调。为了解决一般粗对准方法遇到的问题,开发了一种针对未知初始航向误差的INS误差动态计算方法,并开发了考虑未知航向误差的相应观测方程。第二阶段设计用于精细对准,其中使用基于小姿态误差的经典INS误差动力学。实验结果表明,与常规方法相比,所提出的对准方法可以更快,更准确地完成初始对准。

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