Abstract
Quasi-periodic behavior underlying gravitational three-body dynamics may supply naturally bounded reference trajectories to control spacecraft motion. To insert or maintain a spacecraft into bounded motion that resembles quasi-periodic behavior, guidance algorithms may require target position and velocity values, potentially at a fixed epoch. Within lower fidelity models that are autonomous, Poincaré maps are a particularly effective tool to identify target conditions for nearly quasi-periodic motion; however, challenges remain in transitioning the application of Poincaré maps to higher fidelity models that are nearly time-periodic. In fact, Poincaré maps are often visualized in lower dimensional spaces for inspection; such visualizations do not often supply a static and comprehensive description for the underlying dynamical structures, when dynamics are nearly time-periodic. In this work, we explore a framework to facilitate the interpretation of Poincaré map patterns associated with epoch-dependent solutions and states that are projected to lower dimensional position and velocity spaces. The introduction of chaos indicators may reveal regions of the projection that produce bounded motion as a function of the given epoch and/or initial state perturbation. Within precisely time-periodic systems, these regions may be the image, or shadow, of underlying torus manifolds. In the Poisson sense, shadows of quasi-periodic motion may be considered regions of stability within the lower dimensional space. Within the projection space, chaos indicators may capture time variations of a reference shadow or reveal special perturbation patterns. The framework is presented in two case studies: the first study demonstrates application within binary asteroid dynamics that are precisely time-periodic; the second study demonstrates application within nearly time-periodic dynamics (i.e., an ephemeris representation of the Earth-Moon system), when solutions resemble quasi-periodic motion only over finite time intervals.
![](http://media.springernature.com/m312/springer-static/image/art%3A10.1007%2Fs40295-021-00284-x/MediaObjects/40295_2021_284_Fig1_HTML.png)
![](http://media.springernature.com/m312/springer-static/image/art%3A10.1007%2Fs40295-021-00284-x/MediaObjects/40295_2021_284_Fig2_HTML.png)
![](http://media.springernature.com/m312/springer-static/image/art%3A10.1007%2Fs40295-021-00284-x/MediaObjects/40295_2021_284_Fig3_HTML.png)
![](http://media.springernature.com/m312/springer-static/image/art%3A10.1007%2Fs40295-021-00284-x/MediaObjects/40295_2021_284_Fig4_HTML.png)
![](http://media.springernature.com/m312/springer-static/image/art%3A10.1007%2Fs40295-021-00284-x/MediaObjects/40295_2021_284_Fig5_HTML.png)
![](http://media.springernature.com/m312/springer-static/image/art%3A10.1007%2Fs40295-021-00284-x/MediaObjects/40295_2021_284_Fig6_HTML.png)
![](http://media.springernature.com/m312/springer-static/image/art%3A10.1007%2Fs40295-021-00284-x/MediaObjects/40295_2021_284_Fig7_HTML.png)
![](http://media.springernature.com/m312/springer-static/image/art%3A10.1007%2Fs40295-021-00284-x/MediaObjects/40295_2021_284_Fig8_HTML.png)
![](http://media.springernature.com/m312/springer-static/image/art%3A10.1007%2Fs40295-021-00284-x/MediaObjects/40295_2021_284_Fig9_HTML.png)
![](http://media.springernature.com/m312/springer-static/image/art%3A10.1007%2Fs40295-021-00284-x/MediaObjects/40295_2021_284_Fig10_HTML.png)
![](http://media.springernature.com/m312/springer-static/image/art%3A10.1007%2Fs40295-021-00284-x/MediaObjects/40295_2021_284_Fig11_HTML.png)
![](http://media.springernature.com/m312/springer-static/image/art%3A10.1007%2Fs40295-021-00284-x/MediaObjects/40295_2021_284_Fig12_HTML.png)
![](http://media.springernature.com/m312/springer-static/image/art%3A10.1007%2Fs40295-021-00284-x/MediaObjects/40295_2021_284_Fig13_HTML.png)
![](http://media.springernature.com/m312/springer-static/image/art%3A10.1007%2Fs40295-021-00284-x/MediaObjects/40295_2021_284_Fig14_HTML.png)
![](http://media.springernature.com/m312/springer-static/image/art%3A10.1007%2Fs40295-021-00284-x/MediaObjects/40295_2021_284_Fig15_HTML.png)
![](http://media.springernature.com/m312/springer-static/image/art%3A10.1007%2Fs40295-021-00284-x/MediaObjects/40295_2021_284_Fig16_HTML.png)
![](http://media.springernature.com/m312/springer-static/image/art%3A10.1007%2Fs40295-021-00284-x/MediaObjects/40295_2021_284_Fig17_HTML.png)
![](http://media.springernature.com/m312/springer-static/image/art%3A10.1007%2Fs40295-021-00284-x/MediaObjects/40295_2021_284_Fig18_HTML.png)
![](http://media.springernature.com/m312/springer-static/image/art%3A10.1007%2Fs40295-021-00284-x/MediaObjects/40295_2021_284_Fig19_HTML.png)
![](http://media.springernature.com/m312/springer-static/image/art%3A10.1007%2Fs40295-021-00284-x/MediaObjects/40295_2021_284_Fig20_HTML.png)
![](http://media.springernature.com/m312/springer-static/image/art%3A10.1007%2Fs40295-021-00284-x/MediaObjects/40295_2021_284_Fig21_HTML.png)
![](http://media.springernature.com/m312/springer-static/image/art%3A10.1007%2Fs40295-021-00284-x/MediaObjects/40295_2021_284_Fig22_HTML.png)
![](http://media.springernature.com/m312/springer-static/image/art%3A10.1007%2Fs40295-021-00284-x/MediaObjects/40295_2021_284_Fig23_HTML.png)
![](http://media.springernature.com/m312/springer-static/image/art%3A10.1007%2Fs40295-021-00284-x/MediaObjects/40295_2021_284_Fig24_HTML.png)
Similar content being viewed by others
Notes
currently renamed Artemis-I
References
Arnold, V.: Proof of a theorem of A. N. kolmogorov on the invariance of quasi-periodic motions under small perturbations of the hamiltonian. Russian Mathematical Surveys 18(5), 9–36 (1963). https://doi.org/10.1070/rm1963v018n05abeh004130
Barden, B., Howell, K.: Fundamental motions near collinear libration points and their transitions. Journal of the Astronautical Sciences 46(4), 361–378 (1998)
Baresi, N., Olikara, Z., Scheeres, D.: Survey of numerical methods to compute quasi-periodic invariant tori in astrodynamics. In: AAS/AIAA Space Flight Mechanics Meeting, Napa, California, February (2016)
Baresi, N., Scheeres, D.: Quasi-periodic invariant tori of time-periodic dynamical systems: Applications to small body exploration. In: 67Th International Astronautical Congress, Guadalajara, Mexico, September (2016)
Bennett, C., Bay, M., Halpern, M., Hinshaw, G., Jackson, C., Jarosik, N., Kogut, A., Limon, M., Meyer, S., Page, L., Spergel, D., Tucker, G., Wilkinson, D., Wollack, E., Wright, E.: The Microwave anisotropy probe mission. Astrophys. J. 583(1), 1–23 (2003)
Bester, M., Cosgrove, D., Frey, S., Marchese, J., Burgart, A., Lewis, M., Roberts, B., Thorsness, J., McDonald, J., Pease, D., Picard, G., Eckert, M., Dumlao, R.: ARTEMIS operations - experiences and lessons learned. In: IEEE Aerospace Conference, Big Sky, Montana, March (2014)
Davis, D.C., Phillips, S.M., McCarthy, B.P.: Trajectory design for saturnian ocean worlds orbiters using multidimensional poincaré maps. Acta Astronaut. 143, 16–28 (2018)
Dawn, T., Gutkowski, J., Batcha, A., Pedrotty, S.: Trajectory design considerations for Exploration Mission 1. In: AAS/AIAA Space Flight Mechanics Meeting, Kissimmee, Florida, January. Figure 2 (2018)
Folta, D.C., Pavlak, T.A., Haapala, A.F., Howell, K.C., Woodard, M.A.: Earth–moon libration point orbit stationkeeping: theory, modeling, and operations. Acta Astronaut. 94(1), 421–433 (2014)
Froeschle, C.: Graphical evolution of the Arnold web: from order to chaos. Science 289(5487), 2108–2110 (2000)
Froeschlé, C., Gonczi, R., Lega, E.: The fast Lyapunov indicator: a simple tool to detect weak chaos. Application to the structure of the main asteroidal belt. Planet. Space Sci. 45(7), 881–886 (1997)
Gawlik, E., Marsden, J., Du Toit, P., Campagnola, S.: Lagrangian coherent structures in the planar elliptic restricted three-body problem. Celest. Mech. Dyn. Astron. 103(3), 227–249 (2009)
Geisel, C.: Spacecraft Orbit Design in the Circular Restricted Three-Body Problem Using Higher-Dimensional Poincaré Maps. Ph.D. Dissertation, School of Aeronautics and Astronautics, Purdue University, West Lafayette, Indiana (2013)
Gómez, G., Mondelo, J.: The dynamics around the collinear equilibrium points of the RTBP. Physica D 157(4), 283–321 (2001)
Grebow, D.J., Ozimek, M.T., Howell, K.C., Folta, D.C.: Multibody orbit architectures for lunar south pole coverage. J. Spacecr. Rocket. 45(2), 344–358 (2008)
Guzzetti, D., Zimovan, E., Howell, K., Davis, D.: Stationkeeping Analysis for Spacecraft in Lunar near Rectilinear Halo Orbits. In: AAS/AIAA Space Flight Mechanics Meeting, San Antonio, Texas, February (2017)
Haapala, A.F., Howell, K.C.: Representations of higher-dimensional poincaré maps with applications to spacecraft trajectory design. Acta Astronaut. 96(March), 23–41 (2014)
Haller, G.: A variational theory of hyperbolic lagrangian coherent structures. Physica D: Nonlinear Phenomena 240(7), 574–598 (2011)
Hiday, L.: Optimal Transfers between Libration-Point Orbits in the Elliptic Restricted Three-Body Problem. Ph.D. Dissertation, School of Aeronautics and Astronautics, Purdue University, West Lafayette, Indiana (1992)
Howell, K., Pernicka, H.: Numerical determination of lissajous trajectories in the restricted three-body problem. Celest. Mech. 41(1), 107–124 (1988)
Hussmann, H., Oberst, J., Wickhusen, K., Shi, X., Damme, F., Lüdicke, F., Lupovka, V., Bauer, S.: Stability and evolution of orbits around the binary asteroid 175706 (1996 FG3): Implications for the MarcoPolo-r mission. Planet. Space Sci. 70(1), 102–113 (2012)
Jorba, A.: A numerical study on the existence of stable motions near the triangular points of the real earth-Moon system. A dynamical systems approach to the existence of Trojan motions. Astron. Astrophys. 364(1), 327–338 (2000)
Kolemen, E., Kasdin, J., Gurfil, P.: Quasi-Periodic Orbits of the Restricted Three-Body Problem Made Easy. In: New Trends in Astrodynamics and Applications III, AIP Conference Proceedings, Princeton, New Jersey (2007)
Kolmogorov, A.: On the persistence of conditionally periodic motions under a small change of the Hamilton function. Dokl. Akad. Nauk SSSR, pp. 527–530 (1954)
Larson, W.J., Wertz, J.R.: Space mission analysis and design, 3rd edn. Microcosm, Inc., Torrance, CA (United States) (1992). Figure 2-5
Laskar, J.: The chaotic motion of the solar system: a numerical estimate of the size of the chaotic zones. Icarus 88(2), 266–291 (1990)
Laskar, J.: Frequency analysis for multi-dimensional systems. global dynamics and diffusion. Physica D: Nonlinear Phenomena 67(1-3), 257–281 (1993)
Laskar, J.: Introduction to Frequency Map Analysis, pp 134–150. Springer, Netherlands, Dordrecht (1999)
Lega, E., Froeschlé, C.: Numerical investigations of the structure around an invariant KAM torus using the frequency map analysis. Physica D: Nonlinear Phenomena 95(2), 97–106 (1996)
Lo, M., Williams, B., Bollman, W., Han, D., Hahn, Y., Bell, J., Hirst, E., Corwin, R., Hong, P., Howell, K., Barden, B., Wilson, R.: Genesis mission design. The Journal of Astronautical Sciences 49(1), 169–184 (1998)
Morbidelli, A., Guzzo, M.: The Nekhoroshev Theorem and the Asteroid Belt Dynamical System, pp 107–136. Springer, Netherlands, Dordrecht (1997)
Moser, J.: On invariant curves of area-preserving mappings of an annulus. Nachrichten der Akademie der Wissenschaften in göttingen, Mathematisch-Physikalische 1, 1–20 (1962)
Olikara, Z., Scheeres, D.: Numerical Method for Computing Quasi-Periodic Orbits and Their Stability in the Restricted Three-Body Problem. In: 1St IAA/AAS Conference on the Dynamics and Control of Space Systems, Porto, Portugal, March (2012)
Pavlak, T.: Mission Design Applications in the Earth-Moon System: Transfer Trajectories and Stationkeeping. M.S. Thesis, School of Aeronautics and Astronautics, Purdue University, West Lafayette, Indiana (2010)
Perezpalau, D., Masdemont, J., Gomez, G.: Tools to detect structures in dynamical systems using jet transport. Celest. Mech. Dyn. Astron. 123 (3), 239–262 (2015)
Roberts, C.: Long Term Missions at the Sun-Earth Libration Point L1: ACE, SOHO and WIND. In: AAS/AIAA Astrodynamics Specialist Conference, Girdwood, Alaska, August (2011)
Robutel, P.: Frequency map and global dynamics in the solar system i short period dynamics of massless particles. Icarus 152(1), 4–28 (2001)
Robutel, P., Gabern, F., Jorba, A.: The Observed Trojans and the Global Dynamics Around the Lagrangian Points of the Sun-Jupiter System, pp 53–69. Springer, Netherlands, Dordrecht (2005)
Short, C.: Flow-Informed Strategies for Trajectory Design and Analysis. Ph.D. Dissertation, School of Aeronautics and Astronautics, Purdue University, West Lafayette, Indiana (2016)
Szebehely, V.: Theory of Orbit: The Restricted Problem of Three Bodies. Academic Press, New York (1967)
Tricoche, X., Garth, C., Sanderson, A.: Visualization of topological structures in area-preserving maps. IEEE Trans. Vis. Comput. Graph. 17(12), 1765–1774 (2011)
Villac, B.: Using FLI maps for preliminary spacecraft trajectory design in multi-body environments. Celest. Mech. Dyn. Astron. 102(1-3), 29–48 (2008)
Acknowledgements
This work was completed at Tsinghua University with the support of the 2015 Chinese National Postdoctoral International Exchange Program and the National Natural Science Fund for Distinguished Young Scholars of China (No. 11525208). The authors also would like to thank the anonymous reviewers and Dr. Chappaz for their useful and detailed suggestions.
Author information
Authors and Affiliations
Corresponding author
Ethics declarations
Conflict of Interests
On behalf of all authors, the corresponding author states that there is no conflict of interest.
Additional information
Publisher’s Note
Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.
Rights and permissions
About this article
Cite this article
Guzzetti, D., Baoyin, H. Time-Varying Shadows of Quasi-Periodic Motion Across Sections of the Flow Within Nearly Time-Periodic Three-Body Dynamics. J Astronaut Sci 68, 855–890 (2021). https://doi.org/10.1007/s40295-021-00284-x
Accepted:
Published:
Issue Date:
DOI: https://doi.org/10.1007/s40295-021-00284-x