| タイトル | Variable-structure control of spacecraft attitude maneuvers |
| 著者（英） | Sira-Ramirez, Hebertt; Dwyer, Thomas A. W., III |
| 著者所属（英） | Illinois Univ. |
| 発行日 | 1988-06-01 |
| 言語 | eng |
| 内容記述 | A variable-structure control approach is presented for multiaxial spacecraft attitude maneuvers. Nonlinear sliding surfaces are proposed that result in asymptotically stable, ideal linear decoupled sliding motions of Cayley-Rodrigues attitude parameters, as well as of angular velocities. The resulting control laws are interpreted as more easily implemented and more robust versions of those previously obtained by feedback linearization. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 88A43211 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/370136 |
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