Solar sail cooperative formation flying around L2-type artificial equilibrium points-Reference-Cited by-同舟云学术

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Solar sail cooperative formation flying around L2-type artificial equilibrium points

Published:2020-04 Issue: Volume:169 Page:224-239
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Wang Wei,Baoyin Hexi,Mengali Giovanni,Quarta Alessandro A.

Funder

National Science Fund for Distinguished Young Scholars of China

National Postdoctoral Program for Innovative Talents

China Postdoctoral Science Foundation

University of Pisa

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference71 articles.

1. A Chang’e-4 mission concept and vision of future Chinese lunar exploration activities;Wang;Acta Astronaut.,2016

2. Sunjammer: preliminary end-to-end mission design;Heiligers,2014

3. Novel solar-sail mission concepts for high-latitude Earth and lunar observation;Heiligers;J. Guid. Control Dyn.,2018

4. Design of solar sail trajectories with applications to lunar south pole coverage;Ozimek;J. Guid. Control Dyn.,2009

5. Solar sail trajectories at the lunar L2 Lagrange point;McInnes;J. Spacecr. Rocket.,1993

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