TY  - JOUR
A1  - Renaut, Léo
A1  - Frei, Heike
A1  - Nüchter, Andreas
T1  - Lidar pose tracking of a tumbling spacecraft using the smoothed normal distribution transform
T2  - Remote Sensing
N2  - Lidar sensors enable precise pose estimation of an uncooperative spacecraft in close range. In this context, the iterative closest point (ICP) is usually employed as a tracking method. However, when the size of the point clouds increases, the required computation time of the ICP can become a limiting factor. The normal distribution transform (NDT) is an alternative algorithm which can be more efficient than the ICP, but suffers from robustness issues. In addition, lidar sensors are also subject to motion blur effects when tracking a spacecraft tumbling with a high angular velocity, leading to a loss of precision in the relative pose estimation. This work introduces a smoothed formulation of the NDT to improve the algorithm’s robustness while maintaining its efficiency. Additionally, two strategies are investigated to mitigate the effects of motion blur. The first consists in un-distorting the point cloud, while the second is a continuous-time formulation of the NDT. Hardware-in-the-loop tests at the European Proximity Operations Simulator demonstrate the capability of the proposed methods to precisely track an uncooperative spacecraft under realistic conditions within tens of milliseconds, even when the spacecraft tumbles with a significant angular rate.
KW  - pose tracking
KW  - uncooperative space rendezvous
KW  - lidar
KW  - normal distribution transform
Y1  - 2023
UR  - https://opus.bibliothek.uni-wuerzburg.de/opus4-wuerzburg/frontdoor/index/index/docId/31373
UR  - https://nbn-resolving.org/urn:nbn:de:bvb:20-opus-313738
SN  - 2072-4292
VL  - 15
IS  - 9
ER  -