Investigation of Nonlinear Control Strategies Using GPS Simulator And Spacecraft Attitude Control Simulator

Investigation of Nonlinear Control Strategies Using GPS Simulator And Spacecraft Attitude Control Simulator

In this dissertation, we discuss the Distributed Spacecraft Attitude Control System Simulator (DSACSS) testbed developed at Virginia Polytechnic Institute and State University for the purpose of investigating various control techniques for single and multiple spacecraft. DSACSS is comprised of two i...

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Bibliographic Details
Main Author: Kowalchuk, Scott Allen
Other Authors: Aerospace and Ocean Engineering
Format: Others
Published: Virginia Tech 2014
Subjects:
Sliding Mode Classical Orbital Element Control
Classical Orbital Element Control
Lyapunov Based Spacecraft Attitude Control
Spacecraft Attitude Control
Spacecraft Kinematics and Rigid Body Dynamics
Spacecraft Formation Flying
GPS Hardware-in-the-loop Sim for GN&C
DSACSS
Sliding Mode Spacecraft Attitude Control
Online Access:http://hdl.handle.net/10919/29547
http://scholar.lib.vt.edu/theses/available/etd-11122007-164547/

Internet

http://hdl.handle.net/10919/29547
http://scholar.lib.vt.edu/theses/available/etd-11122007-164547/

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