TY - GEN
T1 - Sensor Fusion using Probabilistic Object Detection for State Estimation
AU - Subedi, Suman
AU - Höhndorf, Lukas
AU - Kulaga, Rafal
AU - Hodaie, Zardosht
AU - Shi, Jun
AU - Fang, Xiang
AU - Holzapfel, Florian
N1 - Publisher Copyright:
© 2023, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2023
Y1 - 2023
N2 - Kalman filtering for global navigation satellite systems (GNSS)-aided inertial navigation has been widely used for state estimation. However, the performance of this technique is highly dependent on the accuracy of the individual sensor measurements - and is limited by the difficulty of modeling of non-linearity for filtering. This has motivated the use of learning-based and hybrid visual-inertial kinematic state estimators using deep learning. However, despite their performance, the deep learning techniques are data inefficient, computationally intensive, and have poor interpretability. We propose an extended Kalman filter (EKF)-based rule-based fusion of visual information with inertial and GNSS measurements. An artificial intelligence (AI)-based probabilistic object detection (POD) algorithm is used to detect (classify and localize) a known landmark, i.e., a landing pad, along with quantifying the semantic and spatial uncertainty of the detection. Monte-Carlo dropout is used to quantify the uncertainties of the object detection. Spatial uncertainty is used as the time-varying statistical noise characteristics for the fusion of the landmark detection. Semantic uncertainty is used to prevent fusion of detections with high uncertainty. Numerical simulations are performed to demonstrate the effectiveness of the proposed method.
AB - Kalman filtering for global navigation satellite systems (GNSS)-aided inertial navigation has been widely used for state estimation. However, the performance of this technique is highly dependent on the accuracy of the individual sensor measurements - and is limited by the difficulty of modeling of non-linearity for filtering. This has motivated the use of learning-based and hybrid visual-inertial kinematic state estimators using deep learning. However, despite their performance, the deep learning techniques are data inefficient, computationally intensive, and have poor interpretability. We propose an extended Kalman filter (EKF)-based rule-based fusion of visual information with inertial and GNSS measurements. An artificial intelligence (AI)-based probabilistic object detection (POD) algorithm is used to detect (classify and localize) a known landmark, i.e., a landing pad, along with quantifying the semantic and spatial uncertainty of the detection. Monte-Carlo dropout is used to quantify the uncertainties of the object detection. Spatial uncertainty is used as the time-varying statistical noise characteristics for the fusion of the landmark detection. Semantic uncertainty is used to prevent fusion of detections with high uncertainty. Numerical simulations are performed to demonstrate the effectiveness of the proposed method.
UR - http://www.scopus.com/inward/record.url?scp=85191427786&partnerID=8YFLogxK
U2 - 10.2514/6.2023-3561
DO - 10.2514/6.2023-3561
M3 - Conference contribution
AN - SCOPUS:85191427786
SN - 9781624107047
T3 - AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023
BT - AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023
Y2 - 12 June 2023 through 16 June 2023
ER -