Bandwidth-limited robust nonlinear spacecraft control

Robust large-angle spacecraft pointing and tracking by Variable Structure Control (VSC) are developed. The control of multiaxial attitude dynamics is a highly nonlinear problem, which can be resolved by exact feedback linearization with respect to attitude variables. This requires exact measurements and perfect model parameters. However, spacecraft maneuvers in uncertain circumstances. Thus robust control is required.

Name thesis:degree_name

Ph.D.

Level thesis:degree_level

Dissertation

Discipline thesis:degree_discipline

Aerospace Engineering

Grantor

University of Illinois at Urbana-Champaign

Year dc:date

2011

Author dc:creator

• Kim, Jinho

Contributors dc:contributor

• Prussing, John E.

• Applied Mechanics
• Engineering, Aerospace
• Engineering, Electronics and Electrical

Statement dc:rights

• Copyright 1991 Kim, Jinho

Language dc:language

eng

Identifier

AAI9124442
(UMI)AAI9124442

OAI identifier oai:identifier

oai:www.ideals.illinois.edu:2142/22466