Optimal Trajectories for Planetary Pole-Sitter Missions
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چکیده
منابع مشابه
Generation of Optimal Trajectories for Earth Hybrid Pole-Sitters
A pole-sitter orbit is a closed path that is constantly above one of the Earth’s poles, by means of continuous low thrust. This work proposes to hybridize solar sail propulsion and solar electric propulsion (SEP) on the same spacecraft, to enable such a pole-sitter orbit. Locally-optimal control laws are found with a semi-analytical inverse method, starting from a trajectory that satisfies the ...
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The pole-sitter concept is a solution to the poor temporal resolution of polar observations from highly inclined, low Earth orbits and the poor high latitude coverage from geostationary orbit. It considers a spacecraft that is continuously above either the North or South Pole and, as such, can provide real-time, continuous and hemispheric coverage of the polar regions. Despite the significant d...
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Low-thrust interplanetary space missions are highly complex and there can be many locally optimal solutions. While several techniques exist to search for globally optimal solutions to low-thrust trajectory design problems, they are typically limited to unconstrained trajectories. The operational design community in turn has largely avoided using such techniques and has primarily focused on accu...
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optimal earth pole-sitter transfers using low-thrust propulsion. Acta Astronautica, 79 . pp. 253-268. ISSN 0094-5765 Copyright © 2012 Elsevier A copy can be downloaded for personal non-commercial research or study, without prior permission or charge Content must not be changed in any way or reproduced in any format or medium without the formal permission of the copyright holder(s) When referrin...
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