The Distributed Spacecraft Attitude Control System Simulator: From Design Concept to Decentralized Control

A spacecraft formation possesses several benefits over a single-satellite mission. However, launching a fleet of satellites is a high-cost, high-risk venture. One way to mitigate much of this risk is to demonstrate hardware and algorithm performance in groundbased testbeds. It is typically difficult...

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Bibliographic Details
Main Author: Schwartz, Jana Lyn
Other Authors: Aerospace and Ocean Engineering
Format: Others
Published: Virginia Tech 2014
Subjects:
Online Access:http://hdl.handle.net/10919/28269
http://scholar.lib.vt.edu/theses/available/etd-07122004-165209/