System characterization and online mass property identification of the SPHERES formation flight testbed

Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2008.

Bibliographic Details
Main Author: Berkovitz, Dustin S. (Dustin Scott)
Other Authors: David W. Miller.
Format: Thesis
Language:eng
Published: Massachusetts Institute of Technology 2008
Subjects:
Online Access:http://hdl.handle.net/1721.1/43083
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author Berkovitz, Dustin S. (Dustin Scott)
author2 David W. Miller.
author_facet David W. Miller.
Berkovitz, Dustin S. (Dustin Scott)
author_sort Berkovitz, Dustin S. (Dustin Scott)
collection MIT
description Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2008.
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spelling mit-1721.1/430832019-04-12T14:45:08Z System characterization and online mass property identification of the SPHERES formation flight testbed System characterization and online mass property identification of the Synchronized Position-Hold, Engage, Reorient Experimental Satellite formation flight testbed Berkovitz, Dustin S. (Dustin Scott) David W. Miller. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Aeronautics and Astronautics. Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2008. Includes bibliographical references (p. 89-91). The National Aeronautics and Space Administration (NASA) and other entities in the aerospace industry have recently been considering distributed architectures for many space applications, such as space-based interferometry. Whether the craft in such a system are structurally connected or flown in tight formation, distribution allows for higher redundancy in case of failures as well as reducing the minimum payload footprint for launch. Designed to fly in precise formation, the SPHERES satellites rely on accurate system characteristics such as thruster strength and vehicle mass and inertia. The SPHERES testbed is described and the applications for formation flight are presented. Mass properties of the SPHERES satellites are examined because of their impact on control determination, with comparison between CAD model estimates and empirically determined values. The sensor and actuator suite, essential for closed-loop control, are also identified and characterized. A recursive least squares algorithm for determining mass properties in real time is explained and implemented both offline and online with results from test flights aboard NASA's KC-135 micro-gravity aircraft (Reduced Gravity Airplane, RGA). by Dustin S. Berkovitz. S.M. 2008-11-07T19:00:12Z 2008-11-07T19:00:12Z 2008 2008 Thesis http://hdl.handle.net/1721.1/43083 244387345 eng M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. http://dspace.mit.edu/handle/1721.1/7582 155 p. application/pdf Massachusetts Institute of Technology
spellingShingle Aeronautics and Astronautics.
Berkovitz, Dustin S. (Dustin Scott)
System characterization and online mass property identification of the SPHERES formation flight testbed
title System characterization and online mass property identification of the SPHERES formation flight testbed
title_full System characterization and online mass property identification of the SPHERES formation flight testbed
title_fullStr System characterization and online mass property identification of the SPHERES formation flight testbed
title_full_unstemmed System characterization and online mass property identification of the SPHERES formation flight testbed
title_short System characterization and online mass property identification of the SPHERES formation flight testbed
title_sort system characterization and online mass property identification of the spheres formation flight testbed
topic Aeronautics and Astronautics.
url http://hdl.handle.net/1721.1/43083
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