Attitude control: A key factor during the design of low-thrust propulsion for CubeSats-Reference-Cited by-同舟云学术

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Attitude control: A key factor during the design of low-thrust propulsion for CubeSats

Published:2020-11 Issue: Volume:176 Page:40-51
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Quinsac Gary^ORCID,Segret Boris,Koppel Christophe,Mosser Benoît^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference48 articles.

1. Cubesat Design specification,2009

2. Nano/microsatellite Market Forecast;SpaceWorks,2019

3. An overview of cube-satellite propulsion technologies and trends;Tummala;Aerospace,2017

4. Space propulsion technology for small spacecraft;Krejci;Proc. IEEE,2018

Cited by 10 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. Lab-on-PCB technology for liquid monopropellant microthrusters: Design, fabrication, and performance evaluation;Sensors and Actuators A: Physical;2024-07

2. Mission analysis of a 1U CubeSat post-mission disposal using a thin-film vacuum arc thruster;Acta Astronautica;2024-06

3. Low-thrust satellite collision avoidance as a minimum-time problem for optimal control;AIAA SCITECH 2024 Forum;2024-01-04

4. Development of a Laser Micro-Thruster and On-Orbit Testing;Aerospace;2023-12-26

5. Magnetic properties of a 3U CubeSat with electric propulsion;Advances in Space Research;2023-10

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