On the advantages of exploiting the hierarchical structure of astrodynamical models. (July 2017)

• Record Type: Journal Article
• Authors: Dei Tos, Diogene Alessandro; Topputo, Francesco
• Is Part Of: Acta astronautica. Volume 136(2017)
• Page Start: 236
• Page End: 247
• Publication Date: 2017-07
• Subjects: n-body dynamics -- Four-body problem -- Three-body problem; Astronautics -- Periodicals; Outer space -- Exploration -- Periodicals; Astronautics; Periodicals; 629.405
• DOI: 10.1016/j.actaastro.2017.02.025
• Languages: English
• ISSNs: 0094-5765

Abstract

Abstract: In this paper an algorithm is developed that combines the capabilities and advantages of several different astrodynamical models of increasing complexity. Splitting these models in a strict hierarchical order yields a clearer grasp on what is available. With the effort of developing a comprehensive model overhead, the equations for the spacecraft motion in simpler models can be readily obtained as particular cases. The proposed algorithm embeds the circular and elliptic restricted three-body problems, the four-body bicircular and concentric models, an averaged n -body model, and, at the top hierarchic ladder, the full ephemeris SPICE-based restricted n -body problem. The equations of motion are reduced to the assignment of 13 time-varying coefficients, which multiply the states and the gravitational potential to reproduce the proper vector field. This approach yields an efficient and quick way to check solutions for different dynamics and parameters. We show that in bottom-up applications, a gradual increase of model complexity benefits accuracy, the chances of success and the convergence rate of a continuation algorithm. Case studies are simple periodic orbits and low-energy transfers. Abstract : Highlights: Astrodynamical models are derived and ordered in a clear hierarchical way. The dynamics is described with 13 time-varying coefficients. A new model, based on averaged coefficients, is proposed. A trajectory refinement algorithm is developed. Results are given for Earth-Moon L1 halo orbits and low-energy transfers.