A high precision attitude determination and control system for the UYS-1 nanosatellite-Reference-Cited by-同舟云学术

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A high precision attitude determination and control system for the UYS-1 nanosatellite

Published:2013-03 Issue: Volume: Page:
ISSN:
Container-title:2013 IEEE Aerospace Conference
language:
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Author:

Chaurais J. R.,Ferreira H. C.,Ishihara J. Y.,Borges R. A.,Kulabukhov A. M.,Larin V. A.,Belikov V. V.

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/6490096/6496810/06496981.pdf?arnumber=6496981

Cited by 4 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. Dynamics Analysis of a Nonlinear Satellite Attitude Control System Using an Exact Linear Model;Mathematics;2023-06-07

2. Design & thermal modeling of solar panel module with embedded reconfigurable Air-Coil for micro-satellites;PLOS ONE;2018-07-31

3. Attitude Control of an Underactuated Satellite Using Two Reaction Wheels;Journal of Guidance, Control, and Dynamics;2015-10

4. Attitude Determination System Based on Vector Observations for Satellites Experiencing Sun-Eclipse Phases;Multibody Mechatronic Systems;2014-08-20

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