Research output: Contribution to journal › Article › peer-review
The spacecraft interacting with the geomagnetic field in electrodynamic mode is subject to parametric perturbations; parameters of the spacecraft are controlled quasi-periodic functions. Under some conditions, there exist control algorithms for spacecraft electrodynamic parameters that allow realizing systems of spacecraft angular position stabilization. Stability of the spacecraft stabilized orientation is proved both analytically and by PC computations.
Original language | English |
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Pages (from-to) | 1333-1344 |
Number of pages | 12 |
Journal | Automation and Remote Control |
Volume | 68 |
Issue number | 8 |
DOIs | |
State | Published - Aug 2007 |
Event | 9th International Seminar on Stability and Oscillations in the Nonlinear Control Systems - Moscow Duration: 31 May 2006 → 2 Jun 2006 |
ID: 29122103