For several proposed configurations of the modular space station, the gravity gradient torque distribution is examined for both Y-POP and inertial hold orbits. The necessary equations are derived to allow for solar panel gimbaling, and a procedure is established which will allow any desired space station configuration to be built up. Results indicated that solar panel gimbaling can be a significant factor in the torque distribution in Y-POP orbits. In addition, for the two configurations that were plotted, bias torque magnitudes varied widely in inertial hold modes. (Author)
Gravity Gradient Torque Profiles over an Orbit for Arbitrary Modular Space Station Configurations in the Y-Pop and Inertial Hold Modes
1972
30 pages
Report
No indication
English
ON SATELLITE ATTITUDE CAPTURING BY THE GRAVITY GRADIENT TORQUE CONDITION AND PASSIVE SAFE HOLD MODE
British Library Conference Proceedings | 2006
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