Quasi-terminator orbits near primitive bodies |
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Authors: | Stephen B. Broschart Gregory Lantoine Daniel J. Grebow |
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Affiliation: | 1. Mission Design and Navigation Section, Jet Propulsion Laboratory, California Institute of Technology, M/S: 301-121, 4800 Oak Grove Dr., Pasadena, CA, 91109, USA
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Abstract: | Quasi-terminator orbits are introduced as a class of quasi-periodic trajectories in the solar radiation pressure (SRP) perturbed Hill dynamics. These orbits offer significant displacements along the Sun-direction without the need for station-keeping maneuvers. Thus, quasi-terminator orbits have application to primitive-body mapping missions, where a variety of observation geometries relative to the Sun (or other directions) can be achieved. This paper describes the characteristics of these orbits as a function of normalized SRP strength and invariant torus frequencies and presents a discussion of mission design considerations for a global surface mapping orbit design. |
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