TY - GEN
T1 - Covariance estimation for GPS-lidar sensor fusion for uavs
AU - Shetty, Akshay
AU - Gao, Grace Xingxin
N1 - Funding Information:
VII. ACKNOWLEDGEMENT The authors would like to sincerely thank Kalmanje Krish-nakumar and his group at NASA Ames for supporting this work under the grant NNX17AC13G.
Publisher Copyright:
© 2017 Institute of Navigation. All rights reserved.
PY - 2017
Y1 - 2017
N2 - Outdoor applications for small-scale Unmanned Aerial Vehicles (UAVs) commonly rely on Global Positioning System (GPS) receivers for continuous and accurate position estimates. However, in urban areas GPS satellite signals might be reflected or blocked by buildings, resulting in multipath or non-line-of-sight (NLOS) errors. In such cases, additional onboard sensors such as Light Detection and Ranging (LiDAR) are desirable. Kalman Filtering and its variations are commonly used to fuse GPS and LiDAR measurements. However, it is important, yet challenging, to accurately characterize the error covariance of the sensor measurements. In this paper, we propose a GPS-LiDAR fusion technique with a novel method for efficiently modeling the position error covariance based on LiDAR point clouds. We model the covariance as a function features distributed in the point cloud. We use the LiDAR point clouds in two ways: To estimate incremental motion by matching consecutive point clouds; and, to estimate global pose by matching with a 3-dimensional (3D) city model. For GPS measurements, we use the 3D city model to eliminate NLOS satellites and model the measurement covariance based on the received signal-To-noise-ratio (SNR) values. Finally, all the above measurements and error covariance matrices are input to an Unscented Kalman Filter (UKF), which estimates the globally referenced pose of the UAV. To validate our algorithm, we conduct UAV experiments in GPS-challenged urban environments on the University of Illinois at Urbana-Champaign campus.
AB - Outdoor applications for small-scale Unmanned Aerial Vehicles (UAVs) commonly rely on Global Positioning System (GPS) receivers for continuous and accurate position estimates. However, in urban areas GPS satellite signals might be reflected or blocked by buildings, resulting in multipath or non-line-of-sight (NLOS) errors. In such cases, additional onboard sensors such as Light Detection and Ranging (LiDAR) are desirable. Kalman Filtering and its variations are commonly used to fuse GPS and LiDAR measurements. However, it is important, yet challenging, to accurately characterize the error covariance of the sensor measurements. In this paper, we propose a GPS-LiDAR fusion technique with a novel method for efficiently modeling the position error covariance based on LiDAR point clouds. We model the covariance as a function features distributed in the point cloud. We use the LiDAR point clouds in two ways: To estimate incremental motion by matching consecutive point clouds; and, to estimate global pose by matching with a 3-dimensional (3D) city model. For GPS measurements, we use the 3D city model to eliminate NLOS satellites and model the measurement covariance based on the received signal-To-noise-ratio (SNR) values. Finally, all the above measurements and error covariance matrices are input to an Unscented Kalman Filter (UKF), which estimates the globally referenced pose of the UAV. To validate our algorithm, we conduct UAV experiments in GPS-challenged urban environments on the University of Illinois at Urbana-Champaign campus.
KW - 3-dimensional (3D) city model
KW - Global positioning system (GPS)
KW - Light detection and ranging (LiDAR)
KW - Unmaned aerial vehicles (UAVs)
KW - Unscented kalman filter (UKF)
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U2 - 10.33012/2017.15165
DO - 10.33012/2017.15165
M3 - Conference contribution
AN - SCOPUS:85047848408
T3 - 30th International Technical Meeting of the Satellite Division of the Institute of Navigation, ION GNSS 2017
SP - 2919
EP - 2923
BT - 30th International Technical Meeting of the Satellite Division of the Institute of Navigation, ION GNSS 2017
PB - Institute of Navigation
T2 - 30th International Technical Meeting of the Satellite Division of the Institute of Navigation, ION GNSS 2017
Y2 - 25 September 2017 through 29 September 2017
ER -