Intersecting invariant manifolds in spatial restricted three-body problems : Design and optimization of Earth-to-halo transfers in the Sun-Earth-Moon scenario
Zanzottera, Anna and Mingotti, Giorgio and Castelli, Roberto and Dellnitz, Michael (2012) Intersecting invariant manifolds in spatial restricted three-body problems : Design and optimization of Earth-to-halo transfers in the Sun-Earth-Moon scenario. Communications in Nonlinear Science and Numerical Simulation, 17 (2). pp. 832-843. ISSN 1007-5704 (https://doi.org/10.1016/j.cnsns.2011.06.032)
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This work deals with the design of transfers connecting LEOs with halo orbits around libration points of the Earth–Moon CRTBP using impulsive maneuvers. Exploiting the coupled circular restricted three-body problem approximation, suitable first guess trajectories are derived detecting intersections between stable manifolds related to halo orbits of EM spatial CRTBP and Earth-escaping trajectories integrated in planar Sun–Earth CRTBP. The accuracy of the intersections in configuration space and the discontinuities in terms of Dv are controlled through the box covering structure implemented in the software GAIO. Finally first guess solutions are optimized in the bicircular four-body problem and single-impulse and two-impulse transfers are presented.
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Item type: Article ID code: 46916 Dates: DateEventFebruary 2012Published5 July 2011Published OnlineSubjects: Technology > Mechanical engineering and machinery
Technology > Motor vehicles. Aeronautics. AstronauticsDepartment: Faculty of Engineering > Mechanical and Aerospace Engineering Depositing user: Pure Administrator Date deposited: 26 Feb 2014 14:36 Last modified: 11 Nov 2024 10:36 Related URLs: URI: https://strathprints.strath.ac.uk/id/eprint/46916