Study on angle-only relative navigation for unmanned aerial vehicle formation in GPS-denied environment

被引:0
|
作者
Zheng, Zixuan [1 ]
Wang, Sha [2 ]
Gong, Baichun [2 ,4 ]
Su, Erlong [3 ]
Huang, Hefei [2 ]
机构
[1] Northwestern Polytech Univ, Sch Astronaut, Xian, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, Coll Astronaut, Nanjing, Peoples R China
[3] China Acad Launch Vehicle Technol, Sci & Technol Space Phys Lab, Beijing, Peoples R China
[4] Nanjing Univ Aeronaut & Astronaut, Coll Astronaut, 29 Yudao St, Nanjing 210016, Jiangsu, Peoples R China
基金
中国国家自然科学基金;
关键词
Unmanned aerial vehicle; consensus-extended Kalman filter; angle-only navigation; observability analysis; LOCALIZATION;
D O I
10.1177/09544100221149235
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
To satisfy the autonomous relative navigation demand of unmanned aerial vehicle (UAV) formation in a GPS-denied environment, an angle-only relative navigation algorithm is proposed. First, the relative states in 3-dimension space are decoupled into relative motion along the horizontal plane and altitude by applying the relative azimuth between the north-east-down global frame and the body-fixed horizontal frame belonging to UAVs. Second, a relative dynamic and measurement model considering the measurement deviation of sensors are established. This solves the problem of colored noise in a majority of sensors used in practical engineering. Third, a consensus constraint model of relative states is established by introducing a geometric constraint among formation members. Additionally, a consensus-extended Kalman filter is designed. Finally, the angle-only relative navigation method is validated using standard Monte Carlo simulations. The simulation results show that all the states of the system are observable when the observability criterion is satisfied. The relative position accuracy achieved using gyros with a drift rate of 50 degrees/h, accelerometers with 1 mg deviation, and optical cameras with 1 degrees Gaussian white noise is within 10 m (3 sigma). Additionally, the method proposed in this study can be used to estimate the sensor measurement deviations effectively. Furthermore, it can be potentially applied to improve the absolute navigation accuracy of UAVs.
引用
收藏
页码:2252 / 2265
页数:14
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