Control of the attitude system for the UMR SAT project
"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, leaf iii.
Landers, Robert G.
Mechanical and Aerospace Engineering
M.S. in Aerospace Engineering
University of Missouri--Rolla
xii, 96 leaves
© 2007 David Randall Walker, All rights reserved.
Thesis - Citation
Library of Congress Subject Headings
Intelligent control systems
Rocket engines -- Thrust
Tethered satellites -- Attitude control systems
Print OCLC #
Link to Catalog Record
Walker, David Randall, "Control of the attitude system for the UMR SAT project" (2007). Masters Theses. 36.