Study for femto satellites using micro control moment gyroscope

Post, Mark and Bauer, Ralf and Li, Junquan and Lee, Regina; (2016) Study for femto satellites using micro control moment gyroscope. In: 2016 IEEE Aerospace Conference. IEEE, USA, pp. 1-8. ISBN 9781479953806 (https://doi.org/10.1109/AERO.2016.7500721)

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Abstract

Abstract— Femto-satellites can be used for distributed space missions that can require hundreds to thousands of satellites for real time, distributed, multi-point networks to accomplish remote sensing and science objectives. While suitable sensors are available using micro-electro-mechanical system technology, most femto-satellite designs have no attitude control capability due to the power and size constraints on attitude control actuators. A novel femto-satellite design that uses a micro-electro-mechanical system Control Moment Gyroscope is studied in this paper. We focus on the principal design, modelling, and discussion of the proposed Control Moment Gyroscope while detailing a controllable femto-satellite design that can make use of attitude control for simple sensing missions.

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  Item type:	Book Section
  ID code:	56918
  Dates:	Date Event 5 March 2016 Published
  Notes:	(c) 2016 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other users, including reprinting/ republishing this material for advertising or promotional purposes, creating new collective works for resale or redistribution to servers or lists, or reuse of any copyrighted components of this work in other works
  Subjects:	Technology > Mechanical engineering and machinery
  Department:	Faculty of Engineering > Design, Manufacture and Engineering Management Faculty of Engineering > Electronic and Electrical Engineering
  Depositing user:	Pure Administrator
  Date deposited:	11 Jul 2016 11:14
  Last modified:	25 Apr 2024 00:06
  URI:	https://strathprints.strath.ac.uk/id/eprint/56918