Abstract

The relative pose estimation of an inactive spacecraft by an active servicer spacecraft is a critical task in the design of current and planned space missions, due to its relevance for close-proximity operations, such as In-Orbit Servicing and Active Debris Removal. This paper introduces a novel framework to enable robust monocular pose estimation for close-proximity operations around an uncooperative spacecraft, which combines a Convolutional Neural Network (CNN) for feature detection with a Covariant Efficient Procrustes Perspective-n-Points (CEPPnP) solver and a Multiplicative Extended Kalman Filter (MEKF). The performance of the proposed method is evaluated at different levels of the pose estimation system. A Single-stack Hourglass CNN is proposed for the feature detection step in order to decrease the computational load of the Image Processing (IP), and its accuracy is compared to the standard, more complex High-Resolution Net (HRNet). Subsequently, heatmaps-derived covariance matrices are included in the CEPPnP solver to assess the pose estimation accuracy prior to the navigation filter. This is done in order to support the performance evaluation of the proposed tightly-coupled approach against a loosely-coupled approach, in which the detected features are converted into pseudomeasurements of the relative pose prior to the filter. The performance results of the proposed system indicate that a tightly-coupled approach can guarantee an advantageous coupling between the rotational and translational states within the filter, whilst reflecting a representative measurements covariance. This suggest a promising scheme to cope with the challenging demand for robust navigation in close-proximity scenarios. Synthetic 2D images of the European Space Agency’s Envisat spacecraft are used to generate datasets for training, validation and testing of the CNN. Likewise, the images are used to recreate a representative close-proximity scenario for the validation of the proposed filter.

Highlights

  • Nowadays, key Earth-based applications such as remote sensing, navigation, and telecommunication, rely on satellite technology on a daily basis

  • This paper introduces a novel framework to estimate the relative pose of an uncooperative target spacecraft with a single monocular camera onboard a servicer spacecraft

  • A method is proposed in which a Convolutional Neural Network (CNN)-based Image Processing (IP) algorithm is combined with a Covariant Efficient Procrustes Perspective-n-Points (CEPPnP) solver and a tightly-coupled Multiplicative Extended Kalman Filter (MEKF) to return a robust estimate of the relative pose as well as of the relative translational and rotational velocities

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Summary

Introduction

Key Earth-based applications such as remote sensing, navigation, and telecommunication, rely on satellite technology on a daily basis. Due to the fact that the trainable features can be selected offline prior to the training, the matching of the extracted feature points with the features of the wireframe model can be performed without the need of a large search space for the image-model correspondences, which usually characterizes most of the edges/corners-based methods [27] In this context, the High-Resolution Net (HRNet) [28] already proved to be a reliable and accurate keypoint detector prior to pose estimation, due to its capability of maintaining a high-resolution representation of the heatmaps through the whole detection process.

Pose estimation framework
Convolutional neural network
Covariance computation
Pose estimation
Navigation filter
Propagation step
Correction step
Reset step
Simulations
Findings
Conclusions and recommendations
Full Text
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