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- W853391408 abstract "SUMMARY One of the sources of torques on near-earth satellites is the interaction of the earth's magnetic field with eddy currents induced in the electrically conducting parts of a spinning satellite. Initially, it is assumed that the geomagnetic field is that of a space-fixed dipole. The equation for the average torque, due to this effect, acting on a satellite of known properties is derived and presented. This equation shows the variation of the torque with the orbital parameters. The time history of the spin vector as influenced by this torque has been investigated. For the general case, the spin vector can be resolved into three orthogonal components which are damped exponentially at three differ- ent rates. The analysis is extended to include the effect of the tilt of the geomag- netic dipole axis with respect to the earth's spin axis. tions which include this effect closely parallel the preceding analysis and equations. The analysis and equa- The generalized parameters, which can be used in analyzing the motion due to eddy currents of any spinning satellite in a near-circular orbit, are pre- sented in graphical form. INTRODUCTION One of the sources of torques on near-earth satellites is the interaction of the earth's magnetic field with eddy currents induced in the electrically conducting parts of a spinning satellite. This effect is considered in refer- ences 1 to" @default.
- W853391408 created "2016-06-24" @default.
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- W853391408 date "1965-04-01" @default.
- W853391408 modified "2023-09-27" @default.
- W853391408 title "Effects of magnetically induced eddy-current torques on spin motions of an earth satellite" @default.
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