Integrated attitude and shape control for OrigamiSats with variable surface reflectivity-Reference-Cited by-同舟云学术

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Integrated attitude and shape control for OrigamiSats with variable surface reflectivity

Published:2023-10 Issue: Volume:211 Page:393-404
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Robb Bonar^ORCID,Russo Aloisia,Soldini Stefania^ORCID,Paoletti Paolo^ORCID,Reveles Juan,Bailet Gilles,McInnes Colin R.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference20 articles.

1. Mechanical design of self-reconfiguring 4D-printed OrigamiSat: A new concept for solar sailing;Russo;Front. Space Technol.,2022

2. Flight status of IKAROS deep space solar sail demonstrator;Tsuda;Acta Astronaut.,2011

3. Controllable propulsion by light: Steering a solar sail via tunable radiation pressure;Ma;Adv. Opt. Mater.,2017

4. Sliding mode control for attitude maneuvers of Helianthus solar sail;Bassetto;Acta Astronaut.,2022

5. Structural response of Helianthus solar sail during attitude maneuvers;Boni;Aerosp. Sci. Technol.,2023

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Design concepts and control algorithm to minimize the control effort for earth-orbit-raising solar sails;Aerospace Science and Technology;2024-03

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