Abstract
Trajectory corrections for lunar flyby transfers to Sun–Earth/Moon libration point orbits (LPOs) with continuous thrusts are investigated using an ephemeris model. The lunar flyby transfer has special geometrical and dynamical structures; therefore, its trajectory correction strategy is considerably different from that of previous studies and should be specifically designed. In this paper, we first propose a control strategy based on the backstepping technique with a dead-band scheme using an ephemeris model. The initial error caused by the launch time error is considered. Since the perturbed transfers significantly diverge from the reference transfers after the spacecraft passes by the Moon, we adopt two sets of control parameters in two portions before and after the lunar flyby, respectively. Subsequently, practical constraints owing to the navigation and propellant systems are introduced in the dynamical model of the trajectory correction. Using a prograde type 2 orbit as an example, numerical simulations show that our control strategy can efficiently address trajectory corrections for lunar flyby transfers with different practical constraints. In addition, we analyze the effects of the navigation intervals and dead-band scheme on trajectory corrections. Finally, trajectory corrections for different lunar flyby transfers are depicted and compared.
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This work was supported by the Canada Research Chair Program under Grant No. 950–230883.
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Yi Qi received his Ph.D. degree in aeronautical and astronautical science and technology from Beihang University, China, in 2017. After three years as a postdoctoral researcher in Ryerson University, he joined Beijing Institute of Technology as an associate professor in 2020. His research area includes orbital dynamics and control for deep space exploration.
Anton de Ruiter received his B.E. degree in mechanical engineering from the University of Canterbury in 1999, and M.A.Sc. and Ph.D. degrees in aerospace engineering from the University of Toronto in 2001 and 2005, respectively. Between 2006 and 2008 he was a visiting research fellow at the Canadian Space Agency in Montreal, and an assistant professor in the Department of Mechanical and Aerospace Engineering at Carleton University from 2009 to 2012. He is currently an associate professor and Canada research chair (Tier 2) in the Department of Aerospace Engineering at Ryerson University in Toronto, Canada. His research interests are in the area of guidance, navigation, and control of aerospace systems.
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Qi, Y., de Ruiter, A. Trajectory correction for lunar flyby transfers to libration point orbits using continuous thrust. Astrodyn 6, 285–300 (2022). https://doi.org/10.1007/s42064-020-0097-2
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DOI: https://doi.org/10.1007/s42064-020-0097-2