Dynamic modeling of the attitude for the MR SAT mission
Keywords and Phrases
"This thesis presents a dynamic model for the attitude of the MR SAT mission. The MR SAT mission is a design project at the University of Missouri - Rolla. This project will study two satellites flying in tethered formation and in controlled free-flying flight. The dynamic model emulates the attitude with environmental disturbances applied to the spacecraft. The effect of the tether tension on the attitude of each spacecraft is also studied"--Abstract, leaf iii.
Mechanical and Aerospace Engineering
M.S. in Aerospace Engineering
University of Missouri--Rolla
xii, 145 leaves
© 2004 Joseph Shaw Stehly, All rights reserved.
Thesis - Citation
Library of Congress Subject Headings
Artificial satellites -- Attitude control systems
Space vehicles -- Attitude control systems
Print OCLC #
Link to Catalog Record
Full-text not available: Request this publication directly from Missouri S&T Library or contact your local library.http://laurel.lso.missouri.edu/record=b5395272~S5
Stehly, Joseph Shaw, "Dynamic modeling of the attitude for the MR SAT mission" (2004). Masters Theses. 3639.
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