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Review Article

Solar sail 𝑯-reversal trajectory: A review of its advances and applications

Xiangyuan Zeng1( )Giovanni Vulpetti2Christian Circi3
School of Automation, Beijing Institute of Technology, Beijing 100081, China
International Academy of Astronautics, Paris 75116, France
Sapienza University of Rome, Rome 00138, Italy
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Abstract

The set of the orbital angular-momentum reversal, or H-reversal, sailcraft trajectory was born as a type of unconventional precursor interstellar mission trajectory by using high-performance solar sails. Starting from an outline of the H-reversal sail trajectory, this paper mainly focuses on the 2D reversal-mode solution to the general solar-photon sail motion equations. The feasible region for H-reversal trajectories in fixed sail attitude angles is illustrated. Some interesting applications of the H-reversal trajectory are presented in detail to show its advantages. As a special case, a precursor interstellar probe can be delivered with a constant sail orientation in the H-reversal trajectory to be compared with the direct-motion sail flyby of the Sun. Of importance are the heliocentric periodic orbits in double H-reversal modes, obtained via both fixed and time-varying sail attitude angles. Two more applications involving H-reversal trajectories are discussed in terms of asteroid deflection and transfer trajectory to rectilinear orbits. Finally, some items of the mathematics behind the 3D motion-reversal trajectories are summarized.

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Astrodynamics
Pages 1-15

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Cite this article:
Zeng X, Vulpetti G, Circi C. Solar sail 𝑯-reversal trajectory: A review of its advances and applications. Astrodynamics, 2019, 3(1): 1-15. https://doi.org/10.1007/s42064-018-0032-y

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Received: 24 February 2018
Accepted: 04 April 2018
Published: 14 December 2018
© Tsinghua University Press 2018