Dynamic modeling of the attitude for the MR SAT mission

Author

Joseph Shaw Stehly

Keywords and Phrases

MR SAT

Abstract

"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, page iii.

Department(s)

Mechanical and Aerospace Engineering

Degree Name

M.S. in Aerospace Engineering

Publisher

University of Missouri--Rolla

Publication Date

Fall 2004

Pagination

xii, 145 pages

Rights

© 2004 Joseph Shaw Stehly, All rights reserved.

Document Type

Thesis - Citation

File Type

text

Language

English

Subject Headings

Artificial satellites -- Attitude control systems
Space vehicles -- Attitude control systems

Thesis Number

T 8661

Print OCLC #

62268549

Link to Catalog Record

Full-text not available: Request this publication directly from Missouri S&T Library or contact your local library.

Recommended Citation

Stehly, Joseph Shaw, "Dynamic modeling of the attitude for the MR SAT mission" (2004). Masters Theses. 3639.
https://scholarsmine.mst.edu/masters_theses/3639