Optimal interplanetary trajectories for Sun-facing ideal diffractive sails

被引:15
作者
Quarta, Alessandro A. [1 ]
Mengali, Giovanni [1 ]
Bassetto, Marco [1 ]
Niccolai, Lorenzo [1 ]
机构
[1] Univ Pisa, Dept Civil & Ind Engn, I-56122 Pisa, Italy
关键词
diffractive solar sail; Sun-facing sail; interplanetary transfer; trajectory optimization; WRINKLING ANALYSIS; SOLAR; MISSION; DESIGN; MODEL;
D O I
10.1007/s42064-023-0158-4
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A diffractive sail is a solar sail whose exposed surface is covered by an advanced diffractive metamaterial film with engineered optical properties. This study examines the optimal performance of a diffractive solar sail with a Sun-facing attitude in a typical orbit-to-orbit heliocentric transfer. A Sun-facing attitude, which can be passively maintained through the suitable design of the sail shape, is obtained when the sail nominal plane is perpendicular to the Sun-spacecraft line. Unlike an ideal reflective sail, a Sun-facing diffractive sail generates a large transverse thrust component that can be effectively exploited to change the orbital angular momentum. Using a recent thrust model, this study determines the optimal control law of a Sun-facing ideal diffractive sail and simulates the minimum transfer times for a set of interplanetary mission scenarios. It also quantifies the performance difference between Sun-facing diffractive sail and reflective sail. A case study presents the results of a potential mission to the asteroid 16 Psyche.
引用
收藏
页码:285 / 299
页数:15
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