| Description |
xii, 145 leaves : illustrations ; 28 cm. |
| Summary |
"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. |
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