A Review of Small UAV Navigation System Based on Multisource Sensor Fusion

被引:16
|
作者
Ye, Xiaoyu [1 ]
Song, Fujun [1 ]
Zhang, Zongyu [1 ]
Zeng, Qinghua [1 ]
机构
[1] Sun Yat Sen Univ, Sch Aeronaut & Astronaut, Shenzhen 518107, Peoples R China
基金
中国国家自然科学基金;
关键词
Sensors; Intelligent sensors; Navigation; Sensor systems; Autonomous aerial vehicles; Aerospace control; Sensor phenomena and characterization; Factor graph optimization (FGO); Kalman filter (KF); multisensor fusion (MSF); resilient; unmanned aircraft systems (UASs); VISUAL-INERTIAL ODOMETRY; KALMAN FILTER; OBSERVABILITY ANALYSIS; COMPLEMENTARY FILTER; MULTISENSOR FUSION; AIDED NAVIGATION; SELF-CALIBRATION; IMU; ROBUST; ATTITUDE;
D O I
10.1109/JSEN.2023.3292427
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
In recent years, unmanned aircraft systems (UASs) have played an increasingly significant role in the military and civil fields. The flight control system, as the "hub" of an unmanned aerial vehicle (UAV), is responsible for the key function of autonomous flight, while a reliable and stable navigation system provides important information such as position status for flight control and represents the "sensory" function of the UAV. A highly autonomous and credible UAV requires a navigation system that meets specific requirements for accuracy, integrity, and continuity, resulting in a multitude of sensors on-board the UAV that are heterogeneous, redundant, and multisource, creating a highly complex navigation system. In this article, we review multisensor fusion (MSF) technology for small UAVs over the last 20 years and provide an overview of three typical multisource fusion architectures based on filtering, factor graph optimization, and data-driven, focusing on inductive identification of key technologies for multisource information fusion state estimation systems, including calibration techniques to improve data quality, observability analysis to provide theoretical support, additional model constraint correction using aircraft, and resilient fusion management techniques across all sources. Finally, we propose future directions for UAS navigation systems to address the limitations of the existing systems.
引用
收藏
页码:18926 / 18948
页数:23
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