Abstract
Close-proximity Coulomb formation flying offers attractive prospects in multiple astronautical missions. A semi-analytical method of constructing the series solution up to an arbitrary order for the relative motion near the equilibrium of Coulomb formation systems is proposed to facilitate the design of Coulomb formations based on a Lindstedt–Poincaré method. The details of the series expansion and coefficient solution for arbitrary \(m\!:\!n\)-period orbits are discussed. To verify the effectiveness of the proposed method, the practical convergence domain of the high-order series solution is computed by comparing it with corresponding numerical solutions that satisfy the specified boundary conditions. Simulation results demonstrate the efficacy of the Lindstedt–Poincaré method in constructing series solutions for the relative motion of Coulomb formation systems.
Similar content being viewed by others
Data availability
The datasets generated during and analyzed during the current study are available from the corresponding author upon reasonable request.
References
King, L.B., Parker, G.G., Deshmukh, S., Chong, J.-H.: Spacecraft formation-flying using inter-vehicle coulomb forces. NIAC Phase I Final Report (2002)
Hughes, J., Schaub, H.: Prospects of using a pulsed electrostatic tractor with nominal geosynchronous conditions. IEEE Trans. Plasma Sci. 45(8), 1887–1897 (2017)
Mullen, E., Gussenhoven, M., Hardy, D., Aggson, T., Ledley, B., Whipple, E.: Scatha survey of high-level spacecraft charging in sunlight. J. Geophys. Res. Space Phys. 91(A2), 1474–1490 (1986)
Whipple, E., Olsen, R.: Importance of differential charging for controlling both natural and induced vehicle potentials on ATS-5 and ATS-6 (1980)
Escoubet, C.P., Fehringer, M., Goldstein, M.: Introduction the cluster mission. Ann. Geophys. 19(10/12), 1197–1200 (2001)
Torkar, K., Nakamura, R., Tajmar, M., Scharlemann, C., Jeszenszky, H., Laky, G., Fremuth, G., Escoubet, C., Svenes, K.: Active spacecraft potential control investigation. Space Sci. Rev. 199(1–4), 515–544 (2016)
Parker, G., Schaub, H., Natarajan, A., King, L.: Coulomb force virtual space structures. In: First Workshop on Innovative System Concepts, vol. 633, pp. 39–44 (2006)
Natarajan, A., Schaub, H.: Linear dynamics and stability analysis of a two-craft coulomb tether formation. J. Guid. Control Dyn. 29(4), 831–839 (2006)
Hogan, E.A., Schaub, H.: Linear stability and shape analysis of spinning three-craft coulomb formations. Celest. Mech. Dyn. Astron. 112(2), 131–148 (2012)
Berryman, J., Schaub, H.: Analytical charge analysis for two-and three-craft coulomb formations. J. Guid. Control. Dyn. 30(6), 1701–1710 (2007)
Inampudi, R., Schaub, H.: Orbit radial dynamic analysis of two-craft coulomb formation at libration points. J. Guid. Control. Dyn. 37(2), 682–691 (2014)
Alikhani, A., Dehghan, M.S., Shafieenejad, I.: Fault tolerant guidance of under-actuated satellite formation flying using inter-vehicle coulomb force. Int. J. Reliab. Risk Saf. Theory Appl. 2(1), 43–52 (2019)
Jones, D. R.: A dynamical systems theory analysis of coulomb spacecraft formations. Ph.D. thesis, Department of Aerospace Engineering, University of Texas at Austin, Austin (2013)
Jones, D.R., Schaub, H.: Collinear three-craft coulomb formation stability analysis and control. J. Guid. Control Dyn. 37(1), 224–232 (2014)
Wang, S.: Patched conic section maneuver trajectory planning for two-craft coulomb formation. IEEE Trans. Aerosp. Electron. Syst. 53(1), 258–272 (2017)
Aslanov, V.S.: Dynamics of a satellite with flexible appendages in the coulomb interaction. J. Guid. Control Dyn. 41(2), 565–572 (2018)
Lin, M., Fu, X., Xu, M., Yan, H.: Coulomb spacecraft formation flying: equilibrium points, periodic orbits, and center manifolds. Phys. D 404, 132357 (2020)
Memon, M.W., Nazari, M., Seo, D., Butcher, E.A.: Fuel efficiency of fully and underconstrained coulomb formations in slightly elliptic reference orbits. IEEE Trans. Aerosp. Electron. Syst. 57(6), 4171–4187 (2021)
Alfriend, K.T., Vadali, S.R., Gurfil, P., How, J.P., Breger, L.: Linear equations of relative motion. In: Spacecraft Formation Flying: Dynamics, Control and Navigation, pp. 83–121. Elsevier, Oxford (2010)
Mostafa, A., El-Saftawy, M.I., Abouelmagd, E.I., López, M.A.: Controlling the perturbations of solar radiation pressure on the Lorentz spacecraft. Symmetry 12(9), 1233 (2020)
Abouelmagd, E.I., Mortari, D., Selim, H.H.: Analytical study of periodic solutions on perturbed equatorial two-body problem. Int. J. Bifurc. Chaos 25(14), 1540040 (2015)
Abouelmagd, E.I., Elshaboury, S.M., Selim, H.H.: Numerical integration of a relativistic two-body problem via a multiple scales method. Astrophys. Space Sci. 361(1), 38 (2016)
Amer, T.S., Abady, I.M.: On the application of KBM method for the 3-D motion of asymmetric rigid body. Nonlinear Dyn. 89, 1591–1609 (2017)
Abouelmagd, E.I.: Periodic solution of the two-body problem by KB averaging method within frame of the modified Newtonian potential. J. Astronaut. Sci. 65(3), 291–306 (2018)
Lakshmikantham, V.: Ordinary differential equations. In: Method of Variation of Parameters for Dynamic Systems, pp. 4–38. Routledge, London (2019)
Liang, Y., Xu, M., Xu, S.: High-order solutions of motion near triangular libration points for arbitrary value of \(\mu \). Nonlinear Dyn. 93, 909–932 (2018)
Marinca, V., Herisanu, N.: Perturbation method: Lindstedt-Poincaré. In: Nonlinear Dynamical Systems in Engineering: Some Approximate Approaches, pp. 9–29. Springer-Verlag, Berlin (2010)
Pal, A.K., Abouelmagd, E.I., García Guirao, J.L., Brzeziński, D.W.: Periodic solutions of nonlinear relative motion satellites. Symmetry 13(4), 595 (2021)
Yamgoué, S.B.: On the harmonic balance with linearization for asymmetric single degree of freedom non-linear oscillators. Nonlinear Dyn. 69(3), 1051–1062 (2012)
Alam, M., Yeasmin, I., Ahamed, M.S.: Generalization of the modified Lindstedt-Poincare method for solving some strong nonlinear oscillators. Ain Shams Eng. J. 10(1), 195–201 (2019)
Lei, H., Xu, B.: High-order analytical solutions around triangular libration points in the circular restricted three-body problem. Mon. Not. R. Astron. Soc. 434(2), 1376–1386 (2013)
Gomez, G., Marcote, M.: High-order analytical solutions of Hill’s equations. Celest. Mech. Dyn. Astron. 94(2), 197–211 (2006)
Masdemont, J.J.: High-order expansions of invariant manifolds of libration point orbits with applications to mission design. Dyn. Syst. 20(1), 59–113 (2005)
Li, Z., Tang, J.: A generalized padé-lindstedt-poincaré method for predicting homoclinic and heteroclinic bifurcations of strongly nonlinear autonomous oscillators. Nonlinear Dyn. 84(3), 1201–1223 (2016)
Belhaq, M., Fiedler, B., Lakrad, F.: Homoclinic connections in strongly self-excited nonlinear oscillators: the Melnikov function and the elliptic Lindstedt-Poincaré method. Nonlinear Dyn. 23(1), 67–86 (2000)
Parker, G.G., King, L.B., Schaub, H.: Steered spacecraft deployment using interspacecraft coulomb forces. In: 2006 American Control Conference. IEEE (2006)
Massari, M., Di Lizia, P., Cavenago, F., Wittig, A.: Differential Algebra software library with automatic code generation for space embedded. In: 2018 AIAA Information Systems-AIAA Infotech Aerospace (2018)
Koon, W.S., Lo, M.W., Marsden, J.E., Ross, S.D.: Construction of trajectories with prescribed itineraries. In: Dynamical Systems, the Three-Body Problem and Space Mission Design, pp. 1167–1181. World Scientific, Singapore (2000)
Acknowledgements
The authors acknowledge the financial support from the Shanghai Sailing Program (21YF1417500).
Funding
The authors have not disclosed any funding.
Author information
Authors and Affiliations
Contributions
ML contributed to the study conception and Methodology and wrote the first draft of the manuscript. JZ contributed to the study conception and carried out project administration. Investigation is performed by MX. XP provided the funding and the support in writing, review and editing. All authors commented on previous versions of the manuscript. All authors read and approved the final manuscript.
Corresponding author
Ethics declarations
Conflict of interest
The authors declare that they have no conflict of interest.
Additional information
Publisher's Note
Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.
Supplementary Information
Below is the link to the electronic supplementary material.
Rights and permissions
Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law.
About this article
Cite this article
Lin, M., Zhang, J., Xu, M. et al. High-order analytical solutions of bounded relative motions for Coulomb formation flying. Nonlinear Dyn 111, 12931–12946 (2023). https://doi.org/10.1007/s11071-023-08518-3
Received:
Accepted:
Published:
Issue Date:
DOI: https://doi.org/10.1007/s11071-023-08518-3