Paper extends reorientation schemes for satellites possessing inertial symmetry about spin-axis, to spinning satellites which are not designed with inertial symmetry; method of torquing described effects changes in spin-axis attitude by plane of satellite; 2-phase attitude control system is developed for asymmetric, spinning earth-satellite which is nominally oriented with its spin axis normal to plane of its orbit.
Two-pulse attitude control of asymmetric spinning satellite
Progress Astronautics Aeronautics
1964
27 pages
Article (Journal)
English
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Magnetic attitude control of spinning satellite
Engineering Index Backfile | 1965
|Attitude Orientation Control for a Spinning Satellite
NTIS | 1991
|Magnetic attitude control of a spinning satellite.
AIAA | 1965
|Attitude orientation control for a spinning satellite
TIBKAT | 1991
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