The equations of motion are developed which describe the dynamic interaction between the spacecraft bus and the movable appendages about a single axis. The effect is evaluated of the dynamic interaction on the attitude control subsystem with computer simulations, and design recommendations to reduce the impact of this interaction on future attitude control subsystems are presented. (Author)
Analysis and Simulation of the Mariner MARS 1971 Scan Platform: Spacecraft Dynamic Interaction
1973
62 pages
Report
Keine Angabe
Englisch
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