The nonlinear attitude motion of gyrostat satellites in a central force field is investigated, with particular emphasis on their long-time dynamic behavior for a wide range of parameters. The numbers of equilibrium solutions, as well as their stability, vary with the rotor speed, and bifurcation dia
โฆ LIBER โฆ
Programmed control of the angular motion of a gyrostat in a central force field
โ Scribed by A. E. Zakrzhevskii
- Publisher
- Springer US
- Year
- 1979
- Tongue
- English
- Weight
- 390 KB
- Volume
- 15
- Category
- Article
- ISSN
- 1573-8582
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