| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 720740 | IFAC Proceedings Volumes | 2007 | 6 Pages |
Abstract
Problems on guidance, onboard signal processing and robust gyromoment motion control of agile spacecraft (SC) for the Earth remote sensing and for the flexible payload transportation, are considered. Elaborated methods for dynamic research of the SC angular motion at principle modes under external and parametric disturbances, partial discrete measurement of the state, multiple filtering and digital control by the gyro moment cluster, are presented
Keywords
Related Topics
Physical Sciences and Engineering
Engineering
Computational Mechanics
Authors
Ye.I. Somov, S.A. Butyrin, S.Ye. Somov,