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Minimum impulse transfers to rotate the line of apsidesTransfer between two coplanar orbits can be accomplished via a single impulse if the two orbits intersect. Optimization of a single-impulse transfer, however, is not possible since the transfer orbit is completely constrained by the initial and final orbits. On the other hand, two-impulse transfers are possible between any two terminal orbits. While optimal scenarios are not known for the general two-impulse case, there are various approximate solutions to many special cases. We consider the problem of an inplane rotation of the line of apsides, leaving the size and shape of the orbit unaffected.
Document ID
20060042655
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Phong, Connie
Sweetser, Theodore H.
Date Acquired
August 23, 2013
Publication Date
August 1, 2005
Subject Category
Astrodynamics
Meeting Information
Meeting: AAS/AIAA Astrodynamics Specialists Conference
Location: Lake Tahoe, CA
Country: United States
Start Date: August 7, 2005
End Date: August 11, 2005
Distribution Limits
Public
Copyright
Other
Keywords
orbit rotation

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