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Embry Riddle Aeronautical University

A Novel Magnetorheological Fluid Damper for a Small Spacecraft with Flexible Appendages

Abstract

dc:description.abstract

<p>Small satellites have become increasingly popular over the past thirty years, particularly since the adoption of the common CubeSat architecture early this century. Because of their restricted volume and electrical budgets however, there are practical limits to the missions that small satellites may adopt. One potential near-term solution to the problem of limited electrical power may be the adoption of larger, flexible solar arrays. However, spacecraft with flexible appendages have historically presented attitude control challenges relating to platform stability given the dynamic response of the flexible components to applied torques. These challenges may be particularly disruptive to a small spacecraft with low inertia. Previous studies have examined minimizing the dynamic motion of flexible appendages via shaping control of the external torquers (attitude actuators), and damping the dynamic responses in various schemes.</p> <p>This thesis presents the possible design of a new damper for the small, flexible spacecraft model. The design takes advantage of a smart material known as a magnetorheological (MR) fluid that was initially created in the 1940s, but has been subject to renewed interest over the past 30 years. A numerical model of the damper system is described and test articles with representative properties are subjected to dynamic testing to inform the model behavior. Completed simulation results for a spacecraft slewing maneuver are presented along with suggestions for future research and future design iterations.</p>

Degree

thesis:*
Name thesis:degree_name
Master of Science in Mechanical Engineering
Level thesis:degree_level
Thesis - Open Access
Discipline thesis:degree_discipline
Mechanical Engineering
Year
2018

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Waelchli, Robert

Subjects

dc:subject × 6

Identifiers

dc:identifier.*
Repository record dc:identifier
https://commons.erau.edu/edt/391
OAI identifier oai:identifier
oai:commons.erau.edu:edt-1390

Chain of custody

source
Harvested from
Embry Riddle Aeronautical University
Base URL
commons.erau.edu/do/oai/
Last updated
2026-07-27
Source record
OAI-PMH GetRecord
citation

Waelchli, Robert. A Novel Magnetorheological Fluid Damper for a Small Spacecraft with Flexible Appendages. Thesis - Open Access thesis, 2018. https://commons.erau.edu/edt/391