Hysteresis Motor Driven One Axis Magnetically Suspended Reaction Sphere

The Attitude and Orbit Control System (AOCS) plays an essential role in the flight control of a spacecraft. This system usually contains a minimum of three reaction wheels (often 4-5 wheels are used for optimization and redundancy). By accelerating the appropriate wheels, the system can produce a ze...

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Main Authors: Zhou, Lei, Nejad, Mohammad Imani, Trumper, David L.
Other Authors: Massachusetts Institute of Technology. Department of Mechanical Engineering
Format: Article
Language:en_US
Published: American Society for Precision Engineering 2015
Online Access:http://hdl.handle.net/1721.1/97730
https://orcid.org/0000-0001-9998-430X
https://orcid.org/0000-0002-8981-1912
https://orcid.org/0000-0001-5358-5450
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author Zhou, Lei
Nejad, Mohammad Imani
Trumper, David L.
author2 Massachusetts Institute of Technology. Department of Mechanical Engineering
author_facet Massachusetts Institute of Technology. Department of Mechanical Engineering
Zhou, Lei
Nejad, Mohammad Imani
Trumper, David L.
author_sort Zhou, Lei
collection MIT
description The Attitude and Orbit Control System (AOCS) plays an essential role in the flight control of a spacecraft. This system usually contains a minimum of three reaction wheels (often 4-5 wheels are used for optimization and redundancy). By accelerating the appropriate wheels, the system can produce a zero-mean reaction torque about any axis to the spacecraft, which enables the spacecraft to maneuver on orbit. Meanwhile, the momentum generated by acceleration can be stored in the wheels.
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spelling mit-1721.1/977302022-10-03T07:51:10Z Hysteresis Motor Driven One Axis Magnetically Suspended Reaction Sphere Zhou, Lei Nejad, Mohammad Imani Trumper, David L. Massachusetts Institute of Technology. Department of Mechanical Engineering Zhou, Lei Nejad, Mohammad Imani Trumper, David L. The Attitude and Orbit Control System (AOCS) plays an essential role in the flight control of a spacecraft. This system usually contains a minimum of three reaction wheels (often 4-5 wheels are used for optimization and redundancy). By accelerating the appropriate wheels, the system can produce a zero-mean reaction torque about any axis to the spacecraft, which enables the spacecraft to maneuver on orbit. Meanwhile, the momentum generated by acceleration can be stored in the wheels. Lincoln Laboratory. Advanced Concepts Committee 2015-07-13T18:32:26Z 2015-07-13T18:32:26Z 2014-11 Article http://purl.org/eprint/type/ConferencePaper http://hdl.handle.net/1721.1/97730 Zhou, Lei, Mohammad Imani Nejad, and David L. Trumper. "Hysteresis Motor Driven One Axis Magnetically Suspended Reaction Sphere." 2014 American Society for Precision Engineering (ASPE) Annual Meeting (November 2014). https://orcid.org/0000-0001-9998-430X https://orcid.org/0000-0002-8981-1912 https://orcid.org/0000-0001-5358-5450 en_US http://aspe.net/publications/Annual_2014/2014%20ASPE%20Proceedings.pdf Proceedings of the 2014 American Society for Precision Engineering (ASPE) Annual Meeting Creative Commons Attribution-Noncommercial-Share Alike http://creativecommons.org/licenses/by-nc-sa/4.0/ application/pdf American Society for Precision Engineering MIT web domain
spellingShingle Zhou, Lei
Nejad, Mohammad Imani
Trumper, David L.
Hysteresis Motor Driven One Axis Magnetically Suspended Reaction Sphere
title Hysteresis Motor Driven One Axis Magnetically Suspended Reaction Sphere
title_full Hysteresis Motor Driven One Axis Magnetically Suspended Reaction Sphere
title_fullStr Hysteresis Motor Driven One Axis Magnetically Suspended Reaction Sphere
title_full_unstemmed Hysteresis Motor Driven One Axis Magnetically Suspended Reaction Sphere
title_short Hysteresis Motor Driven One Axis Magnetically Suspended Reaction Sphere
title_sort hysteresis motor driven one axis magnetically suspended reaction sphere
url http://hdl.handle.net/1721.1/97730
https://orcid.org/0000-0001-9998-430X
https://orcid.org/0000-0002-8981-1912
https://orcid.org/0000-0001-5358-5450
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