Quasi-time-optimal steering law for low-thrust orbit transfer considering angular momentum and torque constraints-Reference-Cited by-同舟云学术

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Quasi-time-optimal steering law for low-thrust orbit transfer considering angular momentum and torque constraints

Published:2021-05 Issue: Volume:182 Page:332-349
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Kitamura Kenji^ORCID,Yamada Katsuhiko^ORCID,Shima Takeya

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference49 articles.

1. The public order of the geostationary orbit: blueprints for the future;Wiessner;Yale J. Int. Law,1983

2. Design of Geosynchronous Spacecraft;Agrawal,1986

3. The Technological and Commercial Expansion of Electric Propulsion in the Past 24 Years;Lev,2017

4. Finding a Way: Boeing's “All Electric Propulsion Satellite”, 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference;Feuerborn,2013

5. Electric Propulsion for Station Keeping and Electric Orbit Raising on Eultelsat Platforms;Casaregola,2015

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1. Solar sail heliocentric transfers with a Q-law;Acta Astronautica;2021-11

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