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Automating Maneuvers: Considerations for Collision Avoidance As more space operators implement large constellations of spacecraft, automating orbit maintenance maneuvers becomes a key feature of their operations concept to ensure that the workload is manageable. However, the practice of performing a maneuver without sharing the plan with other nearby spacecraft causes a risk that two spacecraft will collide, not only destroying the spacecraft involved, but creating debris that will affect all other spacecraft using that orbit regime. In order to share the maneuver plan, a predicted ephemeris file containing the maneuver must be sent to a central authority to screen against predicted trajectories of all other on-orbit objects to determine where and when close approaches will occur that may need to be mitigated. Currently the screening authority used by US operators is the 19th Space Defense Squadron; screenings are performed once every 8 hours, meaning that spacecraft using automated maneuvering need to allow 16 hours to share their maneuver plan via the screening process in advance of maneuver execution in case one screening is missed and the next needs to be used.

In an effort to speed up the screening process to benefit spacecraft using automated maneuvering, a prototype system for performing near-real-time screenings has been developed in support of the NASA Starling mission, a constellation of four cubesats that fly at the same altitude as the SpaceX Starlink constellation. Both of these constellations perform automated maneuvering, so without screening the planned maneuvers before execution, the two constellations would risk a collision. This paper describes the traditional conjunction assessment (CA) process, the prototype real-time CA screening capability, plans for the experiment to test the prototype, and next steps.
Document ID
20240006391
Acquisition Source
Headquarters
Document Type
Conference Paper
Authors
Lauri K. Newman
(National Aeronautics and Space Administration Washington, United States)
Matthew D. Hejduk
(The Aerospace Corporation El Segundo, California, United States)
Date Acquired
May 17, 2024
Subject Category
Astrodynamics
Report/Patent Number
SSC24-V-03
Meeting Information
Meeting: 38th Annual Small Satellite Conference
Location: Logan, UT
Country: US
Start Date: August 3, 2024
End Date: August 8, 2024
Sponsors: Utah State University
Funding Number(s)
CONTRACT_GRANT: 80GSFC19D0011
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
conjunction assessment
autonomous flight dynamics
conjunction
assessment
autonomous
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