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Cislunar Navigation Constellation by Displaced Solar Sails

Published online by Cambridge University Press:  25 May 2017

Xiao Pan  and
Ming Xu
Xiao Pan
Affiliation:
(School of Astronautics, Beihang University, Beijing 100191, China)
Ming Xu*
Affiliation:
(School of Astronautics, Beihang University, Beijing 100191, China)
*
(E-mail: [email protected])
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Abstract

Increasing lunar exploration activities are giving rise to higher demands for a navigation constellation system in cislunar space. A novel constellation of solar sails around the Sun-Earth Artificial Lagrangian Points (ALPs) is proposed for cislunar navigation in this paper, which benefits from the numberless and out-of-plane advantages of ALPs compared with the classical Lagrangian points. To relieve the technical pressure on sail equipment, a two-layer optimisation strategy including the navigation constellation architecture and trajectory design is developed to reduce the desired lightness number of the sail's motion. The constellation architecture is constructed in the shape of a regular tetrahedron, whose size and orientation are derived from the realisable lightness number at the ALPs. The powerful Hamiltonian structure-preserving controller and differential evolution algorithm are adopted to propagate the bounded quasi-periodic trajectory with minimum lightness number variation. With the premise of the sail's high feasibility in the mechanism, the numerical navigation simulations for a typical trans-lunar weak stability boundary trajectory indicate that the proposed navigation constellation has a low geometric dilution of precision factor and a good navigation performance.

Keywords

Solar sailArtificial Lagrangian PointCislunar navigation constellationOptimisation
Type
Research Article
Information
The Journal of Navigation , Volume 70 , Issue 5 , September 2017 , pp. 963 - 982
Copyright
Copyright © The Royal Institute of Navigation 2017 

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