TY - JOUR
T1 - A Fault-Tolerant Cooperative Positioning Approach for Multiple UAVs
AU - Qu, Yaohong
AU - Wu, Jizhi
AU - Xiao, Bing
AU - Yuan, Dongli
N1 - Publisher Copyright:
© 2013 IEEE.
PY - 2017/7/23
Y1 - 2017/7/23
N2 - Due to the increasing potentials and benefits of unmanned aerial vehicles (UAVs) in civil and surveillance applications, the cooperative flight using multiple UAVs has attracted more and more attention. However, fault-tolerant cooperative positioning for malfunctions in global positioning system (GPS) is one of the challenges that need to be addressed in various practical applications of UAVs. Motivated by solving this issue, this paper presents a reliable cooperative positioning approach for multiple UAVs cooperative flight by using the geometric azimuth angle and the inclination angle relative to the reference UAVs. In this proposed cooperative positioning system (COPS), these relative angles are measured through radio direction finding equipped on UAVs. With the horizontal dilution of precision of the various reference UAVs carefully analyzed, the optimal reference UAVs set can be first selected. Based on a constant acceleration kinematic model, an extended Kalman filter is then employed to improve the positioning accuracy. A COPS/GPS fault-tolerant navigation algorithm is finally developed to accommodate GPS fault. Simulation results are further presented to verify that the proposed algorithm can guarantee satisfactory navigation of the UAVs even when their GPS cannot work.
AB - Due to the increasing potentials and benefits of unmanned aerial vehicles (UAVs) in civil and surveillance applications, the cooperative flight using multiple UAVs has attracted more and more attention. However, fault-tolerant cooperative positioning for malfunctions in global positioning system (GPS) is one of the challenges that need to be addressed in various practical applications of UAVs. Motivated by solving this issue, this paper presents a reliable cooperative positioning approach for multiple UAVs cooperative flight by using the geometric azimuth angle and the inclination angle relative to the reference UAVs. In this proposed cooperative positioning system (COPS), these relative angles are measured through radio direction finding equipped on UAVs. With the horizontal dilution of precision of the various reference UAVs carefully analyzed, the optimal reference UAVs set can be first selected. Based on a constant acceleration kinematic model, an extended Kalman filter is then employed to improve the positioning accuracy. A COPS/GPS fault-tolerant navigation algorithm is finally developed to accommodate GPS fault. Simulation results are further presented to verify that the proposed algorithm can guarantee satisfactory navigation of the UAVs even when their GPS cannot work.
KW - Unmanned aerial vehicle
KW - cooperative positioning system
KW - extended Kalman filter
KW - horizontal dilution of precision
UR - http://www.scopus.com/inward/record.url?scp=85028448188&partnerID=8YFLogxK
U2 - 10.1109/ACCESS.2017.2731425
DO - 10.1109/ACCESS.2017.2731425
M3 - 文章
AN - SCOPUS:85028448188
SN - 2169-3536
VL - 5
SP - 15630
EP - 15640
JO - IEEE Access
JF - IEEE Access
M1 - 7990240
ER -