Print Email Facebook Twitter Leveraging neural network uncertainty in adaptive unscented Kalman Filter for spacecraft pose estimation Title Leveraging neural network uncertainty in adaptive unscented Kalman Filter for spacecraft pose estimation Author Pasqualetto Cassinis, L. (TU Delft Space Systems Egineering) Park, Tae Ha (Stanford University) Stacey, Nathan (Stanford University) D'Amico, Simone (Stanford University) Menicucci, A. (TU Delft Space Systems Egineering) Gill, E.K.A. (TU Delft Space Systems Egineering) Ahrns, Ingo (AirBus Defence and Space GmbH) Sanchez-Gestido, Manuel (European Space Agency (ESA)) Date 2023 Abstract This paper introduces an adaptive Convolutional Neural Network (CNN)-based Unscented Kalman Filter for the pose estimation of uncooperative spacecraft. The validation is carried out at Stanford's robotic Testbed for Rendezvous and Optical Navigation on the Satellite Hardware-In-the-loop Rendezvous Trajectories (SHIRT) dataset, which simulates vision-based rendezvous trajectories of a servicer spacecraft to PRISMA's Tango spacecraft. The proposed navigation system is stress-tested on synthetic as well as realistic lab imagery by simulating space-like illumination conditions on-ground. The validation is performed at different levels of the navigation system by first training and testing the adopted CNN on SPEED+, Stanford's spacecraft pose estimation dataset with specific emphasis on domain shift between a synthetic domain and an Hardware-In-the-Loop domain. A novel data augmentation scheme based on light randomization is proposed to improve the CNN robustness under adverse viewing conditions, reaching centimeter-level and 10 degree-level pose errors in 80% of the SPEED+ lab images. Next, the entire navigation system is tested on the SHIRT dataset. Results indicate that the inclusion of a new scheme to adaptively scale the heatmaps-based measurement error covariance based on filter innovations improves filter robustness by returning centimeter-level position errors and moderate attitude accuracies, suggesting that a proper representation of the measurements uncertainty combined with an adaptive measurement error covariance is key in improving the navigation robustness. Subject Active debris removalAdaptive filteringConvolutional neural networksDomain adaptationOn-ground validationRelative pose estimation To reference this document use: http://resolver.tudelft.nl/uuid:991b4cee-257e-4635-96af-fe17a84acf5b DOI https://doi.org/10.1016/j.asr.2023.02.021 ISSN 0273-1177 Source Advances in Space Research, 71 (12), 5061-5082 Part of collection Institutional Repository Document type journal article Rights © 2023 L. Pasqualetto Cassinis, Tae Ha Park, Nathan Stacey, Simone D'Amico, A. Menicucci, E.K.A. Gill, Ingo Ahrns, Manuel Sanchez-Gestido Files PDF 1_s2.0_S0273117723001400_main.pdf 4.2 MB Close viewer /islandora/object/uuid:991b4cee-257e-4635-96af-fe17a84acf5b/datastream/OBJ/view