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Constrained Unscented Particle Filter for SINS/GNSS/ADS Integrated Airship Navigation in the Presence of Wind Field Disturbance

机译:存在风场扰动的SINS / GNSS / ADS联合飞艇导航约束无味粒子滤波器

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摘要

Due to the disturbance of wind field, it is difficult to achieve precise airship positioning and navigation in the stratosphere. This paper presents a new constrained unscented particle filter (UPF) for SINS/GNSS/ADS (inertial navigation system/global navigation satellite system/atmosphere data system) integrated airship navigation. This approach constructs a wind speed model to describe the relationship between airship velocity and wind speed using the information output from ADS, and further establishes a mathematical model for SINS/GNSS/ADS integrated navigation. Based on these models, it also develops a constrained UPF to obtain system state estimation for SINS/GNSS/ADS integration. The proposed constrained UPF uses the wind speed model to constrain the UPF filtering process to effectively resist the influence of wind field on the navigation solution. Simulations and comparison analysis demonstrate that the proposed approach can achieve optimal state estimation for SINS/GNSS/ADS integrated airship navigation in the presence of wind field disturbance.
机译:由于风场的干扰,很难在平流层中实现精确的飞艇定位和导航。本文为SINS / GNSS / ADS(惯性导航系统/全球导航卫星系统/大气数据系统)集成飞艇导航提出了一种新的受限无味粒子滤波器(UPF)。该方法利用从ADS输出的信息构建风速模型来描述飞艇速度与风速之间的关系,并进一步建立SINS / GNSS / ADS组合导航的数学模型。基于这些模型,它还开发了约束UPF以获取SINS / GNSS / ADS集成的系统状态估计。提出的约束UPF使用风速模型约束UPF滤波过程,以有效抵抗风场对导航解的影响。仿真和比较分析表明,该方法可以在风场扰动存在的情况下实现SINS / GNSS / ADS联合飞艇导航的最优状态估计。

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