| Autor: |
Belokonov, I. V., Ivanov, D. S., Ovchinnikov, M. Yu., Pen'kov, V. I. |
| Zdroj: |
Journal of Computer & Systems Sciences International; Sep2019, Vol. 58 Issue 5, p774-785, 12p |
| Abstrakt: |
The angular motion of a nanosatellite equipped with a hysteresis damping system is studied. The required number and sizes of hysteresis rods needed to achieve the specified transient time and aerodynamic orientation with a given accuracy are chosen. Laboratory measurements of parameters of the chosen hysteresis rods are presented. The transient time in the case of abnormal launch of the nanosatellite is estimated. [ABSTRACT FROM AUTHOR] |
| Databáze: |
Complementary Index |
| Externí odkaz: |
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