Control of the attitude system for the UMR SAT project

Author

David Randall Walker

Abstract

"This thesis presents an attitude control model for the UMR SAT project. The UMR SAT project is a student design project at the University of Missouri-Rolla. This project involves the study of two satellites flying in coupled flight as well as formation flight. The control model includes a guidance law using Lyapunov stability principles and a control logic algorithm with the use of both a magnetic coil actuator and thrusters with a throttle filter. A hybrid controller using both magnetic coils and thrusters is also discussed. The magnetic coil controller and thruster controller were synthesized using a dynamic model without perturbations"--Abstract, page iii.

Advisor(s)

Pernicka, Hank

Committee Member(s)

Landers, Robert G.
Krishnamurthy, K.

Department(s)

Mechanical and Aerospace Engineering

Degree Name

M.S. in Aerospace Engineering

Publisher

University of Missouri--Rolla

Publication Date

Spring 2007

Pagination

xii, 96 pages

Note about bibliography

Includes bibliographical references.

Rights

© 2007 David Randall Walker, All rights reserved.

Document Type

Thesis - Citation

File Type

text

Language

English

Subject Headings

Intelligent control systemsMagnetometersRocket engines -- ThrustTethered satellites -- Attitude control systems

Thesis Number

T 9154

Print OCLC #

173493226

Recommended Citation

Walker, David Randall, "Control of the attitude system for the UMR SAT project" (2007). Masters Theses. 36.
https://scholarsmine.mst.edu/masters_theses/36