Magnetic stabilization of a spacecraft and the effect of compensation of information errors |
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| Authors: | A I Tkachenko |
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| Institution: | 1.International Science and Education Center for Information Technologies and Systems,National Academy of Sciences and Ministry of Education and Science,Kiev,Ukraine |
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| Abstract: | The system of spacecraft angular stabilization of middle accuracy rating and with magnetic executive devices is considered.
A three-axis magnetometer is used as a single sensitive element of the subsystem of attitude determination. Combination of
specific features of the control law and the algorithm of attitude determination allows one to realize a sufficiently reliable
stabilization system of simple design, which is rather economical, as far as computing time is concerned. |
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