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Validation of A Simulation Environment for Future Space Traffic ManagementThis study presents initial results of a newly developed simulation environment intendedto explore and assess future Space Traffic Management (STM) scenarios. The number ofnew Resident Space Objects (RSOs) in near-Earth orbit is expected to increase significantlywith the expected future deployment of a number of large constellations. These futurescenarios involve the addition of many tens of thousands of new RSOs, making the analysisinto their impact on collision risk extend beyond what traditional data-mining of present-dayconjunction data can reliably predict. To address this, a robust simulation environment wasdeveloped that implements a full force-model for orbit propagation, and computes continuousall-on-all conjunction statistics for arbitrarily large catalog sizes and simulation timeframes.Collision avoidance and station-keeping maneuvers can be optionally implemented based onconfigurable user inputs including physical characteristics and spacecraft meta-data (e.g.,commercial/government, owner country, etc.). Constellation build-out and de-orbit scenarioswere also implemented and modeled based on real-data analysis. Validation of the simulationresults was a critical component of the simulation development, and was done using the currentcatalog with comparisons against both public and internal NASA data-sets. The comparisonsdemonstrate that, with the appropriate settings, representative levels of conjunction ratesand probabilities can be obtained, providing confidence that the simulation tool can generatemeaningful outcomes for test scenarios. As an initial demonstration of the tool’s capabilities,year-long simulations with station-keeping were conducted to examine conjunction historiesusing both the current object catalog (5800 active satellites) and a hypothetical 60,000 objectscenario involving five potential large constellations. Output metrics include the number ofconjunction events, estimates of collision consequence (fragmentation), delta-V maneuver costs,and the probability of at least one collision occurring. The results highlight the potential thatthe simulation tool has for incorporating and running performance comparisons between, e.g.,various sets of maneuver guidelines, industry norms, and definitions of risk, with the overallobjective of providing actionable data to STM policy makers. The presentation will providean overview of the simulation development and validation efforts, as well as a discussion ofobservations gathered from the initial simulations performed.
Document ID
20230010359
Acquisition Source
Headquarters
Document Type
Conference Paper
Authors
Alaric C Gregoire
(Georgia Institute of Technology Atlanta, Georgia, United States)
Brian C Gunter
(Georgia Institute of Technology Atlanta, Georgia, United States)
Mariel Borowitz
(Georgia Institute of Technology Atlanta, Georgia, United States)
Lauri K Newman
(Goddard Space Flight Center Greenbelt, Maryland, United States)
Matthew D Hejduk
(The Aerospace Corporation El Segundo, California, United States)
Gerald A Schweiger
(Georgia Institute of Technology Atlanta, Georgia, United States)
Date Acquired
July 14, 2023
Subject Category
Astrodynamics
Meeting Information
Meeting: 2023 AAS/AIAA Astrodynamics Specialist Conference
Location: Big Sky, Montana
Country: US
Start Date: August 13, 2023
End Date: August 17, 2023
Sponsors: American Astronautical Society
Funding Number(s)
CONTRACT_GRANT: 22-NUP2022-0043
CONTRACT_GRANT: 80GSFC19F0127
WBS: 144598.01.02.76
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
Single Expert
Keywords
conjunction assessment
space traffic management
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