Periodic orbits for space-based reflectors in the circular restricted three-body problem

Salazar, F.J.T., McInnes, C.R. and Winter, O.C. (2017) Periodic orbits for space-based reflectors in the circular restricted three-body problem. Celestial Mechanics and Dynamical Astronomy, 128(1), pp. 95-113. (doi:10.1007/s10569-016-9739-3)

Salazar, F.J.T., McInnes, C.R. and Winter, O.C. (2017) Periodic orbits for space-based reflectors in the circular restricted three-body problem. Celestial Mechanics and Dynamical Astronomy, 128(1), pp. 95-113. (doi:10.1007/s10569-016-9739-3)

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Abstract

The use of space-based orbital reflectors to increase the total insolation of the Earth has been considered with potential applications in night-side illumination, electric power generation and climate engineering. Previous studies have demonstrated that families of displaced Earth-centered and artificial halo orbits may be generated using continuous propulsion, e.g. solar sails. In this work, a three-body analysis is performed by using the circular restricted three body problem, such that, the space mirror attitude reflects sunlight in the direction of Earth’s center, increasing the total insolation. Using the Lindstedt–Poincaré and differential corrector methods, a family of halo orbits at artificial Sun–Earth L2 points are found. It is shown that the third order approximation does not yield real solutions after the reflector acceleration exceeds 0.245 mm s−2, i.e. the analytical expressions for the in- and out-of-plane amplitudes yield imaginary values. Thus, a larger solar reflector acceleration is required to obtain periodic orbits closer to the Earth. Derived using a two-body approach and applying the differential corrector method, a family of displaced periodic orbits close to the Earth are therefore found, with a solar reflector acceleration of 2.686 mm s−2.

Item Type:Articles
Additional Information:The authors would like to thank the financial support of the FAPESP (São Paulo Research Foundation, Brazil), Grants 2011/08171-3, 2013/03233-6, 2015/00559-3 and the CNPq (National Council for Scientific and Technological Development, Brazil), and the technical support of University of Glasgow. C.R.M was support by a Royal Society Wolfson Research Merit Award.
Status:Published
Refereed:Yes
Glasgow Author(s) Enlighten ID:McInnes, Professor Colin
Authors: Salazar, F.J.T., McInnes, C.R., and Winter, O.C.
College/School:College of Science and Engineering > School of Engineering > Systems Power and Energy
Journal Name:Celestial Mechanics and Dynamical Astronomy
Publisher:Springer
ISSN:0923-2958
ISSN (Online):1572-9478
Published Online:19 November 2016
Copyright Holders:Copyright © 2016 Springer Science+Business Media
First Published:First published in Celestial Mechanics and Dynamical Astronomy 128(1): 95-113
Publisher Policy:Reproduced in accordance with the publisher copyright policy

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