| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 4961511 | Procedia Computer Science | 2017 | 7 Pages |
Abstract
The paper considers comprehensive solution providing functional stability of the spacecraft with changes in its moments of inertia. There was developed the mathematical description of the spacecraft angular position stabilization system (APSS) in the linear and discrete forms. There was shown the process of obtaining spacecraft APSS diagnostic models for the particular kind and class of failure. There was proved possible to diagnose and restore functionality spacecraft APSS at the systemic level, using the regulator coefficients parametric adjustment
Related Topics
Physical Sciences and Engineering
Computer Science
Computer Science (General)
Authors
Vuong Anh Trung, Nguyen Van Thinh,