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Seasonal Variations of the James Webb Space Telescope Orbital DynamicsLV separation state is fixed ECEF, so inertial states vary with hourly, daily, monthly, and yearly frequencies The net effect of all frequencies leads to significant variations in orbit geometry Injection states can be matched with invariant manifolds of periodic orbits in the CR3BP to explain observed final orbit.


Document ID
20150017753
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
Brown, Jonathan (AI Solutions, Inc. Lanham, MD, United States)
Peterson, Jeremy (AI Solutions, Inc. Lanham, MD, United States)
Villac, Benjamin (AI Solutions, Inc. Lanham, MD, United States)
Yu, Wayne (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 11, 2015
Publication Date
August 9, 2015
Subject Category
Astronomy
Report/Patent Number
AAS 15-802
GSFC-E-DAA-TN25129
Report Number: AAS 15-802
Report Number: GSFC-E-DAA-TN25129
Meeting Information
Meeting: 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
Funding Number(s)
CONTRACT_GRANT: NNG14VC09C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Three Body Problem
Launch Windows
James Webb Space Telescope

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