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Orbital Maneuvering System Design and Performance for the Magnetosperic Multiscale FormationOnce in science mission orbits, the four 0.12-km diameter observatories plan to form a tetrahedron with as little as 4-km of separation between spacecraft. The stated operational goal of maneuvering the fleet is no more often than once every two weeks (on average). Derived maneuvering accuracy requirement levied on the ACS
Document ID
20150018420
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
Queen, Steven (NASA Goddard Space Flight Center Greenbelt, MD United States)
Chai, Dean (NASA Goddard Space Flight Center Greenbelt, MD United States)
Placanica, Sam (NASA Goddard Space Flight Center Greenbelt, MD United States)
Date Acquired
September 28, 2015
Publication Date
August 13, 2015
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
GSFC-E-DAA-TN25977
AAS-15-815
Report Number: GSFC-E-DAA-TN25977
Report Number: AAS-15-815
Meeting Information
Meeting: AAS/AIAA Astrodynamics Specialist Conference
Location: Vail, CO
Country: United States
Start Date: August 9, 2015
End Date: August 13, 2015
Sponsors: American Inst. of Aeronautics and Astronautics, American Astronautical Society
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Maneuver and Attitude Dynamics
Formation Flying
Determination and Control

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