Development of robust methods of precision attitude control of small spacecrafts and their implementation at the problem-oriented processors

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Spacecraft Dynamics and Control
1Kuntsevich, VM, 2Palagin, OV, 3Gubarev, VF, 4Babii, NА, 3Volosov, VV, 2Lisovyi, OM, 3Melnychuk, SV, 2Opanasenko, VM, 3Shevchenko, VM
1Space Research Institute of the National Academy of Sciences of Ukraine and the National Space Agency of Ukraine, Kyiv, Ukraine
2V. M. Glushkov Institute of Cybernetics of the National Academy of Science of Ukraine, Kyiv, Ukraine
3Space Research Institute of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine, Kyiv, Ukraine
4Space Research Institute of the National Academy of Science of Ukraine and the National Space Agency of Ukraine, Kyiv, Ukraine
Kosm. nauka tehnol. 2015, 21 ;(1):03–09
https://doi.org/10.15407/knit2015.01.003
Publication Language: Russian
Abstract: 

The work is devoted to the adaptation of robust ellipsoidal state estimation methods for dynamic systems to the changes of attitude control of small spacecrafts. Software and hardware implementation of these methods at the problem-oriented processors in FPGAs element basis is established. Its effectiveness is illustrated by the example of the attitude control system of small spacecraft, when a three-axis magnetometer is using as a measuring device.
Keywords: attitude control, ellipsoid method, problem oriented processor, small spacecraft
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