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Design of Quasi-Terminator Orbits near Primitive BodiesQuasi-terminator orbits are a class of quasi-periodic orbits around a primitive body that exist in the vicinity of the well-known terminator orbits. The inherent stability of quasi-terminator trajectories and their wide variety of viewing geometries make them a very compelling option for primitive body mapping missions. In this paper, we discuss orbit design methodologies for selection of an appropriate quasi-terminator orbit that would meet the needs of a specific mission. Convergence of these orbits in an eccentric, higher-fidelity model is also discussed with an example case at Bennu, the target of the upcoming NASA's OSIRIS-REx mission.
Document ID
20150008068
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Lantoine, Gregory
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Broschart, Stephen B.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Grebow, Daniel J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
May 13, 2015
Publication Date
August 11, 2013
Subject Category
Lunar And Planetary Science And Exploration
Report/Patent Number
AAS 13-815
Meeting Information
Meeting: AAS/AIAA Astrodynamics Specialist Conference
Location: Hilton Head, SC
Country: United States
Start Date: August 11, 2013
End Date: August 15, 2013
Sponsors: American Astronautical Society, American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Other
Keywords
mapping
comets
visible spectrum
Hayabusa spacecraft
MarcoPolo
asteroids
Rosetta
OSIRIS

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