Solar Sail Augmented Hohmann Transfer

被引：4

作者：

Quarta, Alessandro A. ^{[1
,2
]}

Mengali, Giovanni ^{[1
]}

Niccolai, Lorenzo ^{[1
]}

Bianchi, Christian ^{[1
]}

机构：

[1] Univ Pisa, Pisa, Italy

[2] Univ Pisa, Dept Civil & Ind Engn, I-56122 Pisa, Italy

来源：

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 2023年 / 59卷 / 02期

关键词：

Propulsion; Orbits; Trajectory; Space vehicles; Sun; Mathematical models; Chemicals; Hohmann transfer; hybrid propulsion system; solar sail; trajectory optimization; TRAJECTORY DESIGN; FORCE MODEL; PERFORMANCE;

D O I：

10.1109/TAES.2022.3206727

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The aim of this correspondence is to analyze the performance of a solar sail-based spacecraft in a two-impulse orbit transfer between circular and coplanar heliocentric orbits of assigned radii. In particular, assuming a transfer trajectory with a sweep angle and a flight time equal to those of a classical Hohmann orbit, the sail propulsive acceleration is used to minimize the total velocity variation required by the two tangential impulses. In this sense, the article quantifies the optimal performance of a solar sail augmented Hohmann transfer as a function of the sail characteristics.

引用

页码：2065 / 2071

页数：7

共 38 条

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[Anonymous], 1976, ASTR C, DOI DOI 10.2514/6.1976-792

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