In this paper, we revisit the classical problem of attitude tracking for a rigid body. The interesting di erence in the formulation is the assumption that only attitude measurements are available. We proceed to construct globally stabilizing control laws in terms of a minimal set of three-dimensiona
β¦ LIBER β¦
Bounded Output Feedback of Rigid-Body Attitude via Angular Velocity Observers
β Scribed by Hu, Jinchang; Zhang, Honghua
- Book ID
- 121233095
- Publisher
- American Institute of Aeronautics and Astronautics
- Year
- 2013
- Tongue
- English
- Weight
- 745 KB
- Volume
- 36
- Category
- Article
- ISSN
- 0731-5090
- DOI
- 10.2514/1.57187
No coin nor oath required. For personal study only.
π SIMILAR VOLUMES
Rigid body attitude tracking without ang
β
Maruthi R. Akella
π
Article
π
2001
π
Elsevier Science
π
English
β 125 KB
Output feedback stabilization of the ang
β
A. Astolfi
π
Article
π
1999
π
Elsevier Science
π
English
β 294 KB
Robust output feedback stabilization of
β
F. Mazenc; A. Astolfi
π
Article
π
2000
π
Elsevier Science
π
English
β 109 KB
The problem of semi-global stabilization of the angular velocity of an underactuated rigid body in the presence of model errors is addressed and solved using a smooth, time-varying, dynamic, output feedback control law. The proposed scheme improves some of the existing results and provides guideline
PD+ Based Output Feedback Attitude Contr
β
Schlanbusch, R.; Loria, A.; Kristiansen, R.; Nicklasson, P. J.
π
Article
π
2012
π
IEEE
π
English
β 331 KB
Hybrid attitude tracking of rigid bodies
β
Rune Schlanbusch; Esten Ingar GrΓΈtli; Antonio Loria; Per Johan Nicklasson
π
Article
π
2012
π
Elsevier Science
π
English
β 332 KB
Global feedback stabilization of the ang
β
Valeria Andriano
π
Article
π
1993
π
Elsevier Science
π
English
β 242 KB