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Fully Safe Rendezvous Strategy in Cis-Lunar Space: Passive and Active Collision Avoidance.

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Název: Fully Safe Rendezvous Strategy in Cis-Lunar Space: Passive and Active Collision Avoidance.
Autoři: Bucchioni, Giordana, De Benedetti, Matteo, D'Onofrio, Fabio, Innocenti, Mario
Zdroj: Journal of the Astronautical Sciences; Oct2022, Vol. 69 Issue 5, p1319-1346, 28p
Témata: THREE-body problem, LAGRANGIAN points, ORBITAL assembly of space vehicles, ORBITS (Astronomy), MOTION capture (Human mechanics)
Abstrakt: The future assembly of the Lunar Orbital Platform Gateway, on a near 9:2 resonant Rectilinear Halo Orbit, requires the necessity of designing safe and reliable strategies to perform rendezvous and docking with the station. The paper describes and tests a strategy to guarantee the safety of an entire rendezvous manoeuvre in the proximity of the Moon L2 Lagrangian point with respect to a specific set of failures. The safety in the far range is guaranteed through the automatic allocation of selected hold-points, whereas during close range rendezvous the safety is actively guaranteed in the presence of selected failures. The main goal of the paper is to contribute to the very limited literature about autonomous design of the guidance for rendezvous in presence of a non negligible third body influence, where safety considerations are paramount. The proposed approach is based on the exploitation of the manifold theory used in the circular restricted three body problem model to guarantee the passive safety in the far-range section, and on an optimal and reliable active collision avoidance manoeuvre to guarantee the safety for the close range approach. [ABSTRACT FROM AUTHOR]
Copyright of Journal of the Astronautical Sciences is the property of Springer Nature and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.)
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  Data: Fully Safe Rendezvous Strategy in Cis-Lunar Space: Passive and Active Collision Avoidance.
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  Data: <searchLink fieldCode="AR" term="%22Bucchioni%2C+Giordana%22">Bucchioni, Giordana</searchLink><br /><searchLink fieldCode="AR" term="%22De+Benedetti%2C+Matteo%22">De Benedetti, Matteo</searchLink><br /><searchLink fieldCode="AR" term="%22D'Onofrio%2C+Fabio%22">D'Onofrio, Fabio</searchLink><br /><searchLink fieldCode="AR" term="%22Innocenti%2C+Mario%22">Innocenti, Mario</searchLink>
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  Data: Journal of the Astronautical Sciences; Oct2022, Vol. 69 Issue 5, p1319-1346, 28p
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  Label: Abstract
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  Data: The future assembly of the Lunar Orbital Platform Gateway, on a near 9:2 resonant Rectilinear Halo Orbit, requires the necessity of designing safe and reliable strategies to perform rendezvous and docking with the station. The paper describes and tests a strategy to guarantee the safety of an entire rendezvous manoeuvre in the proximity of the Moon L2 Lagrangian point with respect to a specific set of failures. The safety in the far range is guaranteed through the automatic allocation of selected hold-points, whereas during close range rendezvous the safety is actively guaranteed in the presence of selected failures. The main goal of the paper is to contribute to the very limited literature about autonomous design of the guidance for rendezvous in presence of a non negligible third body influence, where safety considerations are paramount. The proposed approach is based on the exploitation of the manifold theory used in the circular restricted three body problem model to guarantee the passive safety in the far-range section, and on an optimal and reliable active collision avoidance manoeuvre to guarantee the safety for the close range approach. [ABSTRACT FROM AUTHOR]
– Name: Abstract
  Label:
  Group: Ab
  Data: <i>Copyright of Journal of the Astronautical Sciences is the property of Springer Nature and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract.</i> (Copyright applies to all Abstracts.)
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        Value: 10.1007/s40295-022-00339-7
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      – Code: eng
        Text: English
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        Type: general
      – SubjectFull: LAGRANGIAN points
        Type: general
      – SubjectFull: ORBITAL assembly of space vehicles
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      – TitleFull: Fully Safe Rendezvous Strategy in Cis-Lunar Space: Passive and Active Collision Avoidance.
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            – D: 01
              M: 10
              Text: Oct2022
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              Y: 2022
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