Abstract
This paper considers the problem of constructing time-optimal trajectories for a spacecraft (SC) with a solar sail. The trajectories under consideration consist of repeated cycles of spacecraft movement to the target heliocentric orbit and back to the initial one. A model of a perfectly reflecting sail is used, which allows using the programs for optimal control of the sail angle, obtained on the basis of the Pontryagin maximum principle. The heliocentric motion is modeled in a flat polar coordinate system, and the spacecraft itself makes cyclic flights between two terrestrial planets along a closed trajectory. A boundary-value problem is formulated, in the solution of which the approach of the spacecraft to the target planet with the equalization of velocities is ensured (the encounter problem). Simulations of four cycles of Earth–Mercury–Earth and Earth–Mars–Earth motion with a characteristic acceleration of the solar sail of 0.25 mm/s2 have been carried out, for which the duration of one cycle is on average 2000 and 2341 days, respectively. Optimal sail-orientation control programs are obtained for a wide range of launch dates, and methods of searching for and choosing the initial values of conjugate variables are shown. The obtained results demonstrate the ability of a spacecraft with a solar sail to implement controlled motion along closed trajectories with a minimum duration of individual Earth–destination planet–Earth flights.
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REFERENCES
Sinyavskii, V.V., Scientific and technical groundwork for the Hercules nuclear electric rocket interorbital tug, Kosm. Tekh. Tekhnol., 2013, no. 3, pp. 25–45.
Crusan, J.C., Smith, R.M., Craig, D.A., et al., Deep space gateway concept: Extending human presence into cislunar space, Proc. IEEE Aerospace Conference, 2018, vol. 2018. https://doi.org/10.1109/AERO.2018.8396541
Haws, T.D., Zimmerman, J.S., and Fuller, M.E., SLS, the gateway, and a lunar outpost in the early 2030s, Proc. IEEE Aerospace Conference, 2019, vol. 2019. https://doi.org/10.1109/AERO.2019.8741598
Polyakhova, E.N., Kosmicheskii polet s solnechnym parusom: problemy i perspektivy (Space Flight with a Solar Sail: Problems and Prospects), Moscow: Nauka, 1986.
Mel’nikov, V.M., Matyushenko, I.N., Chernova, N.A., et al., Problems of creating large-sized structures in space, Tr. Mosk. Aviats. Inst., 2014, no. 78, pp. 1–21.
Mori, O., Sawada, H., Funase, R., et al., First solar power sail demonstration by IKAROS, Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, 2010, vol. 8, no. 27, pp. 25–31. https://doi.org/10.2322/tastj.8.To_4_25
Spencer, D.A., Betts, B., Bellardo, J.M., et al., The LightSail 2 solar sailing technology demonstration, Adv. Space Res., 2021, vol. 67, no. 9, pp. 2878–2889. https://doi.org/10.1016/j.asr.2020.06.029
Frisbee, R.H., Solar sails for Mars cargo missions, AIP Conf. Proc., 2007, vol. 374, pp. 374–380.
Hughes, G.W., Macdonald, M., McInnes, C.R., et al., Sample return from Mercury and other terrestrial planets using solar sail propulsion, J. Spacecr. Rockets, 2006, vol. 43, no. 4, pp. 828–835.
Vergaaij, M. and Heiligers, J., Time-optimal solar sail heteroclinic-like connections for an Earth–Mars cycler, Acta Astronaut., 2018, vol. 152, pp. 474–485.
Pontryagin, L.S., Boltyanskii, V.G., Gamkrelidze, R.V., et al., Matematicheskaya teoriya optimal’nykh protsessov (Mathematical Theory of Optimal Processes), Moscow: Nauka, 1969.
Du, Ch. and Starinova, O.L., Generation of artificial halo orbits in near-Moon space using low-thrust engines, Cosmic Res., 2022, vol. 60, no. 2, pp. 151–166. https://doi.org/10.31857/S0023420622020029
Wright, J.L., Space Sailing, Philadelphia: Gordon and Breach Science Publishers, 1992.
McInnes, C.R., Solar Sailing: Technology, Dynamics and Mission Applications, Berlin: Springer, 2004.
Vulpetti, G., Johnson, L., and Matloff, G.L., Solar Sails: A Novel Approach to Interplanetary Travel, New York: Springer, 2015.
Beletskii, V.V., Egorov, V.A., and Ershov, V.G., Analysis of trajectories of interplanetary flights with engines of constant power, Kosm. Issled., 1965, vol. 3, no. 4, pp. 507–522.
Ishkov, S.A., Milokumova, O.L., and Salmin, V.V., Optimization of closed interplanetary Earth–Mars–Earth with low thrust, Kosm. Issled., 1995, vol. 33, no. 2, pp. 210–219.
Forward, R.L., Grey solar sails, J. Astronaut. Sci., 1989, vol. 38, no. 2, pp. 161–185.
Rozhkov, M.A., Influence of the optical characteristics of a multilayer solar sail on its heliocentric motion, Vestn. Samar. Univ. Aerokosm. Tekh., Tekhnol. Mashinostr., 2022, vol. 21, no. 4, pp. 52–65. https://doi.org/10.18287/2541-7533-2022-21-4-52-65
Zhukov, A.N. and Lebedev, V.N., Variational problem of a flight between heliocentric circular orbits with the help of a solar sail, Kosm. Issled., 1964, vol. 2, no. 1, pp. 46–50.
Starinova, O.L., Raschet mezhplanetnykh pereletov kosmicheskikh apparatov s maloy tyagoy (Calculation of Interplanetary Transfers of Low-Thrust Spacecraft), Samara: Izd. Samar. Nauchn. Tsentra RAN, 2007.
Starinova, O.L., Sergaeva, E.A., and Rozhkov, M.A., RF Patent 2022617890, 2022.
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Rozhkov, M.A., Starinova, O.L. Optimization of Solar-Sail Control When a Vehicle Moves along Cyclic Heliocentric Trajectories. Cosmic Res 61, 534–543 (2023). https://doi.org/10.1134/S0010952523700430
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DOI: https://doi.org/10.1134/S0010952523700430