Abstract
Investigation of new orbit geometries exhibits a very attractive behavior for a spacecraft to monitor space weather coming from the Sun. Several orbit transfer mechanisms are analyzed as potential alternatives to monitor solar activity such as a sub-solar orbit or quasi-satellite orbit and short and long heteroclinic and homoclinic connections between the triangular points L4 and L5 and the collinear point L3 of the Circular Restricted Three-Body Problem (CRTBP) in the Sun-Earth system.
Original language | American English |
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State | Published - Aug 2013 |
Event | AAS/AIAA Astrodynamics Specialist Conference - Hilton Head, SC Duration: Aug 1 2013 → … |
Conference
Conference | AAS/AIAA Astrodynamics Specialist Conference |
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Period | 8/1/13 → … |
Keywords
- Sun-Earth system
- spacecraft orbit
- triangular points L4 and L5
Disciplines
- Space Vehicles