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This technical note presents a practical approach to low-energy Earth–Moon transfer autonomous guidance considering high-fidelity orbital dynamics. Initially, autonomous guidance, delineated as a trajectory-tracking problem, is addressed within the framework of a predesigned reference trajectory solution, accompanied by empirical trajectory correction maneuver allocation. A series of two-point boundary value problems is subsequently formulated to incorporate guidance velocity increments. An algorithm employing quasilinearization, discretization, and recursion is proposed to address these boundary value problems, which results in enhanced convergence performance compared with traditional differential-correction-based guidance methods. Finally, a Monte Carlo analysis demonstrates the efficacy of the proposed autonomous guidance approach, indicating its potential for onboard applications.
Trageser, M. B., Hoag, D. G. Apollo spacecraft guidance system. IFAC Proceedings Volumes, 1965, 2(1): 435–463.
Yin, Y. C., Wang, M., Shi, Y., Zhang, H. Midcourse correction of Earth–Moon distant retrograde orbit transfer trajectories based on high-order state transition tensors. Astrodynamics, 2023, 7(3): 335–349.
Hill, K., Born, G. H. Autonomous interplanetary orbit determination using satellite-to-satellite tracking. Journal of Guidance, Control, and Dynamics, 2007, 30(3): 679–686.
Turan, E., Speretta, S., Gill, E. Autonomous navigation for deep space small satellites: Scientific and technological advances. Acta Astronautica, 2022, 193: 56–74.
Von Stryk, O., Bulirsch, R. Direct and indirect methods for trajectory optimization. Annals of Operations Research, 1992, 37(1): 357–373.
Wang, Z. B., Grant, M. J. Optimization of minimum-time low-thrust transfers using convex programming. Journal of Spacecraft and Rockets, 2018, 55(3): 586–598.
Wang, Z. B., Grant, M. J. Autonomous entry guidance for hypersonic vehicles by convex optimization. Journal of Spacecraft and Rockets, 2018, 55(4): 993–1006.
Ortolano, N., Geller, D. K., Avery, A. Autonomous optimal trajectory planning for orbital rendezvous, satellite inspection, and final approach based on convex optimization. The Journal of the Astronautical Sciences, 2021, 68(2): 444–479.
Dueri, D., Açıkmeşe, B., Scharf, D. P., Harris, M. W. Customized real-time interior-point methods for onboard powered-descent guidance. Journal of Guidance, Control, and Dynamics, 2017, 40(2): 197–212.
Hofmann, C., Topputo, F. Rapid low-thrust trajectory optimization in deep space based on convex programming. Journal of Guidance, Control, and Dynamics, 2021, 44(7): 1379–1388.
Mammarella, M., Capello, E., Park, H., Guglieri, G., Romano, M. Tube-based robust model predictive control for spacecraft proximity operations in the presence of persistent disturbance. Aerospace Science and Technology, 2018, 77: 585–594.
Sachan, K., Padhi, R. Waypoint constrained multi-phase optimal guidance of spacecraft for soft lunar landing. Unmanned Systems, 2019, 7(2): 83–104.
Hong, H. C., Maity, A., Holzapfel, F., Tang, S. J. Model predictive convex programming for constrained vehicle guidance. IEEE Transactions on Aerospace and Electronic Systems, 2019, 55(5): 2487–2500.
Shin, J. Adaptive dynamic surface control for a hypersonic aircraft using neural networks. IEEE Transactions on Aerospace and Electronic Systems, 2017, 53(5): 2277–2289.
LaFarge, N. B., Miller, D., Howell, K. C., Linares, R. Autonomous closed-loop guidance using reinforcement learning in a low-thrust, multi-body dynamical environment. Acta Astronautica, 2021, 186: 1–23.
Gaudet, B., Linares, R., Furfaro, R. Deep reinforcement learning for six degree-of-freedom planetary landing. Advances in Space Research, 2020, 65(7): 1723–1741.
Newton, I. The Principia: The Authoritative Translation and Guide. California: University of California Press, 1999: 125–127.
Dei Tos, D. A., Rasotto, M., Renk, F., Topputo, F. LISA Pathfinder mission extension: A feasibility analysis. Advances in Space Research, 2019, 63(12): 3863–3883.
Howell, K. C., Pernicka, H. J. Numerical determination of Lissajous trajectories in the restricted three-body problem. Celestial Mechanics, 1987, 41(1): 107–124.
Marchand, B. G., Howell, K. C., Wilson, R. S. Improved corrections process for constrained trajectory design in the n-body problem. Journal of Spacecraft and Rockets, 2007, 44(4): 884–897.
Marchand, B. G., Weeks, M. W., Smith, C. W., Scarritt, S. Onboard autonomous targeting for the trans-earth phase of Orion. Journal of Guidance, Control, and Dynamics, 2010, 33(3): 943–956.
Feng, H. Y., Wang, X. C., Yue, X. K., Wang, C. T. A survey of computational methods for spacecraft orbit propagation and Lambert problems. Acta Aeronautica et Astronautica Sinica 2023, 44(13): 028027.
Montenbruck, O., Gill, E., Lutze, F. Satellite Orbits: Models, Methods and Applications. New York: Springer-Verlag Berlin Heidelberg, 2000: 53–83.
Huang, C., Jin, W., Xu, H. The terrestrial and lunar reference frame in lunar laser ranging. Journal of Geodesy, 1999, 73(3): 125–129.
Peng, C., Zhang, H., Wen, C. X., Zhu, Z. F., Gao, Y. Exploring more solutions for low-energy transfers to lunar distant retrograde orbits. Celestial Mechanics and Dynamical Astronomy, 2022, 134(1): 4.
Zhang, C., Zhang, H. Lunar-gravity-assisted low-energy transfer from Earth into Distant Retrograde Orbit (DRO). Acta Aeronautica et Astronautica Sinica 2023, 44(2): 326507.
Morrison, D. D., Riley, J. D., Zancanaro, J. F. Multiple shooting method for two-point boundary value problems. Communications of the ACM, 1962, 5(12): 613–614.
Bai, X. L., Junkins, J. L. Modified Chebyshev-Picard iteration methods for solution of boundary value problems. The Journal of the Astronautical Sciences, 2011, 58(4): 615–642.
Boyd, J. P. Chebyshev and Fourier Spectral Methods, 2nd edn. New York: Springer-Verlag Berlin Heidelberg, 2000: 109–123.
Chen, Q. F., Zhang, Y. D., Liao, S. Y., Wan, F. L. Newton–Kantorovich/pseudospectral solution to perturbed astrodynamic two-point boundary-value problems. Journal of Guidance, Control, and Dynamics, 2013, 36(2): 485–498.
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