From Design to Deorbit: A Solar-Electric Autonomous Module for Multi-Debris Remediation

Fuente: arXiv
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Main Authors: Mishra, Om, Patil, Jayesh, Narkedimilli, Sathwik, Sharma, G Srikantha, S, Ananda, Vanahalli, Manjunath K
Format: Preprint
Published: 2026
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author Mishra, Om
Patil, Jayesh
Narkedimilli, Sathwik
Sharma, G Srikantha
S, Ananda
Vanahalli, Manjunath K
author_facet Mishra, Om
Patil, Jayesh
Narkedimilli, Sathwik
Sharma, G Srikantha
S, Ananda
Vanahalli, Manjunath K
contents The escalating accumulation of orbital debris threatens the sustainability of space operations, necessitating active removal solutions that overcome the limitations of current fuel-dependent methods. To address this, this study introduces a novel remediation architecture that integrates a mechanical clamping system for secure capture with a high-efficiency, solar-powered NASA Evolutionary Xenon Thruster (NEXT) and autonomous navigation protocols. High-fidelity simulations validate the architecture's capabilities, demonstrating a successful retrograde deorbit from 800 km to 100 km, <10m position Root Mean Square Errors (RMSE) via radar-based Extended Kalman Filter (EKF) navigation, and a 93\% data delivery efficiency within 1 second using Delay/Disruption Tolerant Network (DTN) protocols. This approach significantly advances orbital management by establishing a benchmark for renewable solar propulsion that minimizes reliance on conventional fuels and extends mission longevity for multi-target removal.
format Preprint
id arxiv_https___arxiv_org_abs_2601_12830
institution arXiv
publishDate 2026
record_format arxiv
spellingShingle From Design to Deorbit: A Solar-Electric Autonomous Module for Multi-Debris Remediation
Mishra, Om
Patil, Jayesh
Narkedimilli, Sathwik
Sharma, G Srikantha
S, Ananda
Vanahalli, Manjunath K
Distributed, Parallel, and Cluster Computing
Robotics
The escalating accumulation of orbital debris threatens the sustainability of space operations, necessitating active removal solutions that overcome the limitations of current fuel-dependent methods. To address this, this study introduces a novel remediation architecture that integrates a mechanical clamping system for secure capture with a high-efficiency, solar-powered NASA Evolutionary Xenon Thruster (NEXT) and autonomous navigation protocols. High-fidelity simulations validate the architecture's capabilities, demonstrating a successful retrograde deorbit from 800 km to 100 km, <10m position Root Mean Square Errors (RMSE) via radar-based Extended Kalman Filter (EKF) navigation, and a 93\% data delivery efficiency within 1 second using Delay/Disruption Tolerant Network (DTN) protocols. This approach significantly advances orbital management by establishing a benchmark for renewable solar propulsion that minimizes reliance on conventional fuels and extends mission longevity for multi-target removal.
title From Design to Deorbit: A Solar-Electric Autonomous Module for Multi-Debris Remediation
topic Distributed, Parallel, and Cluster Computing
Robotics
url https://arxiv.org/abs/2601.12830