A Low-Cost UAV Swarm Relative Positioning Architecture Based on BDS/Barometer/UWB

被引:0
|
作者
Zhang, Shuning [1 ]
Wang, Ershen [2 ,3 ]
Wang, Yongkang [2 ]
Yu, Tengli [1 ]
Jia, Shiyu [4 ]
Xu, Song [2 ]
Qu, Pingping [2 ]
机构
[1] Shenyang Aerosp Univ, Coll Aeronaut & Astronaut, Shenyang 110136, Peoples R China
[2] Shenyang Aerosp Univ, Coll Elect Informat Engn, Shenyang 110136, Peoples R China
[3] Shenyang Aerosp Univ, Coll Civil Aviat, Shenyang 110136, Peoples R China
[4] China Elect Technol Grp Corp, Res Inst 54, Shijiazhuang 050081, Hebei, Peoples R China
基金
中国国家自然科学基金;
关键词
BeiDou system (BDS); cooperative positioning; gradient descent algorithm; integrated navigation; ultrawideband (UWB); unmanned aerial vehicle (UAV) swarm;
D O I
10.1109/JSEN.2024.3476286
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
The issue of relative positioning in unmanned aerial vehicle (UAV) swarms is critical for effective cooperative management and network construction. However, the current low-cost BeiDou system (BDS) exhibits poor accuracy, typically ranging from several meters to tens of meters, which fails to meet the basic requirements for cooperative positioning. To address this challenge, a combined positioning architecture based on BDS, barometer, and ultrawideband (UWB), alongside an accuracy optimization algorithm using gradient descent, is proposed. First, existing UAV swarm positioning technologies and algorithms are analyzed. By combining data from BDS, barometer, and UWB sensors, the accuracy problem of the combined system was transformed into an optimization problem. Then, models such as data credibility evaluation, information difference calculation, and gradient descent optimization were used to solve the optimization problem. Finally, a precision-optimized BDS/barometer/UWB-combined positioning architecture is proposed. Simulations and real-world experiments demonstrate that the fusion positioning architecture achieves higher cooperative positioning accuracy compared to mainstream systems, such as inertial navigation systems (INSs) and BDS. The final distance root mean square error (RMSE) is reduced to 1.313 m, a 69.0% improvement over the 4.231 m observed with standalone BDS.
引用
收藏
页码:39659 / 39668
页数:10
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