| タイトル | Inversion Of Dynamical Equations For Control Of Attitude |
| 著者（英） | Paielli, Russell; Bach, Ralph |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1995-10-01 |
| 言語 | eng |
| 内容記述 | Method of inverting nonlinear equations of rotational dynamics of rigid body used to design feedback control of orientation of body. Applicable to both direction-cosine and quaternion formulations suitable for large-angle maneuvers. Exploiting some apparently little-known properties of direction cosine and quaternion formulations, method leads to equations for model-follower control system that exhibits exactly linear attitude-error dynamics. Quarternion system more robust in responding to large roll-angle commands. |
| NASA分類 | MECHANICS |
| レポートNO | 95B10533
ARC-12769 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/305547 |
