Angle of arrival-based target localisation with low Earth orbit satellite observer

被引:6
|
作者
Norouzi, Yaser [1 ]
Kashani, Elham Sadat [1 ]
Ajorloo, Abdollah [2 ]
机构
[1] Amirkabir Univ Technol, Dept Elect Engn, Tehran, Iran
[2] Sharif Univ Technol, Dept Elect Engn, Tehran, Iran
来源
IET RADAR SONAR AND NAVIGATION | 2016年 / 10卷 / 07期
关键词
direction-of-arrival estimation; Earth; artificial satellites; singular value decomposition; satellite navigation; angle of arrival-based target localisation; low Earth orbit satellite observer; triangulation target localisation method; Earth surface; flat plate; low-altitude observer; high-altitude observer; LEO satellite observer; spherical surface; spherical trigonometry; SVD; error bound; TDOA; BIAS;
D O I
10.1049/iet-rsn.2015.0437
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 triangulation (or angle of arrival) target localisation method, the surface of the Earth is approximated by a flat plate. This approximation, while acceptable for low-altitude observers (such as unmanned aerial vehicles), is not a correct model for high-altitude observers (such as low Earth orbit - LEO satellites). In this study, the authors have discussed triangulation method using a LEO satellite observer over a spherical surface and have shown that, using spherical trigonometry and singular value decomposition (SVD), a straight forward solution can be found for target localisation problem. Also, error bound is discussed and analysed using both SVD as well as simulation.
引用
收藏
页码:1186 / 1190
页数:5
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