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A Quaternion-Based Adaptive Attitude Tracking Controller Without Velocity Measurements'
| Content Provider | Semantic Scholar |
|---|---|
| Author | Kapiliat, V. |
| Copyright Year | 2000 |
| Abstract | The main problem addressed in this paper is the quaternion-based, attitude tracking control of rigid spacecraft without angular velocity measurements and in the presence of an unknown inertia matrix. As a stepping-stone, we first de- sign an adaptive, full-state feedback controller that compensates for parametric uncertainty while ensuring asymptotic attitude tracking errors. The adaptive, full-state feedback controller is then redesigned such that the need for angular velocity measure- ments is eliminated. The proposed adaptive, output feedback controller ensures asymptotic attitude tracking. |
| File Format | PDF HTM / HTML |
| Alternate Webpage(s) | http://aldebaran.elo.utfsm.cl/datasheet/cdc/cdc00/PDF/AUTHOR/CD001094.PDF |
| Language | English |
| Access Restriction | Open |
| Content Type | Text |
| Resource Type | Article |