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   <subfield code="a">Three-dimensional time Optimal Multi-reversal Orbit by Using Solar Sailing</subfield>
   <subfield code="h">[Elektronische Daten]</subfield>
   <subfield code="c">[Xiangyuan Zeng, Kyle Alfriend, S. Vadali]</subfield>
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   <subfield code="a">In this paper a new family of three dimensional (3D) non-Keplerian orbits is produced by using ideally reflective solar sailing. A sailcraft departs from the Earth orbit to accomplish a novel periodic orbit with orbital angular momentum reversing four times over one period. Such a new kind of orbit is referred to as the &quot;multi-reversal orbit”. It is symmetrical with respect to the plane which contains the Sun-perihelion line. This property benefits the calculations and reduces the simulation effort. In order to find the minimum periodic orbits, a time optimal control model is constructed and solved by using an indirect method. Two typical 3D multi-reversal orbits are obtained with different orbital constraints. Some orbital characteristic, like quasi-heliostationary condition near its two aphelion points, are demonstrated via numerical simulations. A comparison between these two typical orbits is conducted to show more details about this new orbit. Differences between the multi-reversal orbit and double-reversal orbit are presented to show the advantages of the multi-reversal concept.</subfield>
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   <subfield code="a">Zeng</subfield>
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   <subfield code="t">The Journal of the Astronautical Sciences</subfield>
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