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首页> 外文期刊>Mathematical Problems in Engineering: Theory, Methods and Applications >A Novel Fusion Scheme for Vision Aided Inertial Navigation of Aerial Vehicles
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A Novel Fusion Scheme for Vision Aided Inertial Navigation of Aerial Vehicles

机译:飞行器视觉辅助惯性导航的新型融合方案

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Vision-aided inertial navigation is an important and practical mode of integrated navigation for aerial vehicles. In this paper, a novel fusion scheme is proposed and developed by using the information from inertial navigation system (INS) and vision matching subsystem. This scheme is different from the conventional Kalman filter (CKF); CKF treats these two information sources equally even though vision-aided navigation is linked to uncertainty and inaccuracy. Eventually, by concentrating on reliability of vision matching, the fusion scheme of integrated navigation is upgraded. Not only matching positions are used, but also their reliable extents are considered. Moreover, a fusion algorithm is designed and proved to be the optimal as it minimizes the variance in terms of mean square error estimation. Simulations are carried out to validate the effectiveness of this novel navigation fusion scheme. Results show the new fusion scheme outperforms CKF and adaptive Kalman filter (AKF) in vision/INS estimation under given scenarios and specifications.
机译:视觉辅助惯性导航是飞行器集成导航的重要且实用的模式。本文利用惯性导航系统(INS)和视觉匹配子系统的信息,提出并提出了一种新颖的融合方案。该方案与传统的卡尔曼滤波器(CKF)不同。即使视觉辅助导航与不确定性和不准确性相关,CKF也会同等对待这两个信息源。最终,通过专注于视觉匹配的可靠性,集成导航的融合方案得以升级。不仅使用匹配位置,而且考虑其可靠程度。此外,设计了一种融合算法,并证明它是最佳的,因为它在均方误差估计方面将方差最小化。进行仿真以验证这种新颖的导航融合方案的有效性。结果表明,在给定场景和规格下,新的融合方案在视觉/ INS估计方面优于CKF和自适应卡尔曼滤波器(AKF)。

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