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通过基于CDGNSS/视觉的协同导航改进飞行中惯性偏差估计

Improved In-Flight Estimation of Inertial Biases through CDGNSS/Vision Based Cooperative Navigation.

作者信息

Causa Flavia, Fasano Giancarmine

机构信息

Department of Industrial Engineering, University of Naples Federico II, Piazzale Tecchio 80, 80125 Naples, Italy.

出版信息

Sensors (Basel). 2021 May 14;21(10):3438. doi: 10.3390/s21103438.

Abstract

This paper discusses the exploitation of a cooperative navigation strategy for improved in-flight estimation of inertial sensors biases on board unmanned aerial vehicles. The proposed multi-vehicle technique is conceived for a "chief" Unmanned Aerial Vehicle (UAV) and relies on one or more deputy aircrafts equipped with Global Navigation Satellite System (GNSS) antennas for differential positioning which also act as features for visual tracking. Combining carrier-phase differential GNSS and visual estimates, it is possible to retrieve accurate inertial-independent attitude information, thus potentially enabling improved bias estimation. Camera and carrier-phase differential GNSS measurements are integrated within a 15 states extended Kalman filter. Exploiting an ad hoc developed numerical environment, the paper analyzes the performance of the cooperative approach for inertial biases estimation as a function of number of deputies, formation geometry and distances, and absolute and relative dynamics. It is shown that exploiting two deputies it is possible to improve biases estimation, while a single deputy can be effective if changes of relative geometry and dynamics are also considered. Experimental proofs of concept based on two multi-rotors flying in formation are presented and discussed. The proposed framework is applicable beyond the domain of small UAVs.

摘要

本文讨论了一种协同导航策略的应用,该策略用于改进无人机机载惯性传感器偏差的飞行中估计。所提出的多飞行器技术是为“主”无人机(UAV)设计的,它依赖于一个或多个配备全球导航卫星系统(GNSS)天线的副飞行器进行差分定位,这些副飞行器也作为视觉跟踪的特征。结合载波相位差分GNSS和视觉估计,可以获取精确的与惯性无关的姿态信息,从而有可能实现改进的偏差估计。相机和载波相位差分GNSS测量值被集成到一个15状态的扩展卡尔曼滤波器中。利用专门开发的数值环境,本文分析了协同方法用于惯性偏差估计的性能,该性能是副飞行器数量、编队几何形状和距离以及绝对和相对动力学的函数。结果表明,利用两个副飞行器可以改进偏差估计,而如果也考虑相对几何形状和动力学的变化,单个副飞行器也可能有效。本文给出并讨论了基于两个编队飞行的多旋翼飞行器的概念验证实验。所提出的框架适用于小型无人机领域之外。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/997b/8157035/9892fe4511d7/sensors-21-03438-g001.jpg

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