Application of a magnetohydrodynamic element in the control loop of a rotating spacecraft with cavities partially filled with liquid
| Autor: | A. I. Mytarev, R. R. Nazirov, B. I. Rabinovich |
|---|---|
| Rok vydání: | 2008 |
| Předmět: |
Physics
Spacecraft business.industry Aerospace Engineering Astronomy and Astrophysics Rocket propellant Gyroscope Mechanics law.invention Attitude control Loop (topology) Classical mechanics Space and Planetary Science law Control system Physics::Space Physics Magnetohydrodynamic drive Magnetohydrodynamics business |
| Zdroj: | Cosmic Research. 46:251-263 |
| ISSN: | 1608-3075 0010-9525 |
| DOI: | 10.1134/s001095250803009x |
| Popis: | This paper is a continuation of [1–3] and a generalization of the results for a rotating spacecraft with cavities partially filled with liquid and equipped with an operational magnetohydrodynamic (MHD) element in the loop of its attitude control. This element makes possible the creation of hingeless systems of stabilization and orientation that do not require rocket propellant consumption. The application of an MHD element is considered for stabilization in the mode of spin-up of a spacecraft not having gyroscopic stability. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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