Optical system design for a multi-CubeSats debris surveillance mission

The detection and observation of space debris in Low Earth Orbit is generally carried out through the use of ground based radars and telescopes. These instruments allow for a precise reconstruction of the space debris trajectories, and therefore represent a key asset for planning avoidance maneuvers...

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Main Authors: Pineau, Dan, Felicetti, Leonard
Format: Conference Object
Language:English
Published: International Astronautical Federation (IAF) 2022
Subjects:
Online Access:https://iac2022.org/
https://dspace.lib.cranfield.ac.uk/handle/1826/18470
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author Pineau, Dan
Felicetti, Leonard
author_facet Pineau, Dan
Felicetti, Leonard
author_sort Pineau, Dan
collection Cranfield University: Collection of E-Research - CERES
description The detection and observation of space debris in Low Earth Orbit is generally carried out through the use of ground based radars and telescopes. These instruments allow for a precise reconstruction of the space debris trajectories, and therefore represent a key asset for planning avoidance maneuvers when threats of collisions are predicted. The recent deployment of mega-constellations, with the consequent increase of the number of satellites, imposes new challenges in terms of simultaneous tracking capability and readiness of the current space situational awareness systems. This adds to the current need to track small and dull objects to further mitigate the probability of triggering cascade collisions. However, ground based observations are limited due to their intrinsic sensibility to atmospheric refraction, their diurnal inoperability and their dependence on meteorological hazards. This paper proposes to study the feasibility and the benefits of a potential deployment of a constellation of CubeSats in Low Earth Orbit, to acquire optical observations of space debris with enhanced accuracy, as part of the ORCA mission: Orbit Refinement for Collision Avoidance. Here, the focus is on the optical design of the payload instrument to be integrated onboard of the orbiting platforms. The study trades-off the current state-of-art of optical detection technologies, by assessing their performance against a set of specific requirements: (a) the minimization of the uncertainty associated to the image resolution; (b) a field of view that maximizes the extent of the monitored area; (c) an optimal exposure time to avoid under or overexposure of the image; (d) minimization of the effects of light diffraction and above all, (e) the maximization of the signal to noise ratio to detect the smallest and dullest objects possible. Real observations of space debris are conducted to validate the models. Several configurations of optical systems are then chosen as suitable for the ORCA constellation, also considering the system design ...
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Pineau D, Felicetti L (2022) Optical system design for a multi-CubeSats debris surveillance mission. In: 73rd International Astronautical Congress (IAC-22), 18-22 September 2022, Paris, France
https://iac2022.org/
https://dspace.lib.cranfield.ac.uk/handle/1826/18470
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spelling ftcranfield:oai:dspace.lib.cranfield.ac.uk:1826/18470 2025-01-17T00:10:01+00:00 Optical system design for a multi-CubeSats debris surveillance mission Pineau, Dan Felicetti, Leonard 2022-09-22 https://iac2022.org/ https://dspace.lib.cranfield.ac.uk/handle/1826/18470 en eng International Astronautical Federation (IAF) IAC-22,B4,7,2,x71408 Pineau D, Felicetti L (2022) Optical system design for a multi-CubeSats debris surveillance mission. In: 73rd International Astronautical Congress (IAC-22), 18-22 September 2022, Paris, France https://iac2022.org/ https://dspace.lib.cranfield.ac.uk/handle/1826/18470 Attribution 4.0 International http://creativecommons.org/licenses/by/4.0/ CC-BY space debris optical system CubeSats design requirements constellation Conference Paper 2022 ftcranfield 2023-02-09T23:38:47Z The detection and observation of space debris in Low Earth Orbit is generally carried out through the use of ground based radars and telescopes. These instruments allow for a precise reconstruction of the space debris trajectories, and therefore represent a key asset for planning avoidance maneuvers when threats of collisions are predicted. The recent deployment of mega-constellations, with the consequent increase of the number of satellites, imposes new challenges in terms of simultaneous tracking capability and readiness of the current space situational awareness systems. This adds to the current need to track small and dull objects to further mitigate the probability of triggering cascade collisions. However, ground based observations are limited due to their intrinsic sensibility to atmospheric refraction, their diurnal inoperability and their dependence on meteorological hazards. This paper proposes to study the feasibility and the benefits of a potential deployment of a constellation of CubeSats in Low Earth Orbit, to acquire optical observations of space debris with enhanced accuracy, as part of the ORCA mission: Orbit Refinement for Collision Avoidance. Here, the focus is on the optical design of the payload instrument to be integrated onboard of the orbiting platforms. The study trades-off the current state-of-art of optical detection technologies, by assessing their performance against a set of specific requirements: (a) the minimization of the uncertainty associated to the image resolution; (b) a field of view that maximizes the extent of the monitored area; (c) an optimal exposure time to avoid under or overexposure of the image; (d) minimization of the effects of light diffraction and above all, (e) the maximization of the signal to noise ratio to detect the smallest and dullest objects possible. Real observations of space debris are conducted to validate the models. Several configurations of optical systems are then chosen as suitable for the ORCA constellation, also considering the system design ... Conference Object Orca Cranfield University: Collection of E-Research - CERES
spellingShingle space debris
optical system
CubeSats
design requirements
constellation
Pineau, Dan
Felicetti, Leonard
Optical system design for a multi-CubeSats debris surveillance mission
title Optical system design for a multi-CubeSats debris surveillance mission
title_full Optical system design for a multi-CubeSats debris surveillance mission
title_fullStr Optical system design for a multi-CubeSats debris surveillance mission
title_full_unstemmed Optical system design for a multi-CubeSats debris surveillance mission
title_short Optical system design for a multi-CubeSats debris surveillance mission
title_sort optical system design for a multi-cubesats debris surveillance mission
topic space debris
optical system
CubeSats
design requirements
constellation
topic_facet space debris
optical system
CubeSats
design requirements
constellation
url https://iac2022.org/
https://dspace.lib.cranfield.ac.uk/handle/1826/18470