Name
Abstract | ||
|---|---|---|
In this brief, a tracking controller is presented to stabilize the attitude of a micro satellite via integrator backstepping and quaternion feedback. The controller is shown to render the equilibrium points in the closed-loop system uniformly asymptotically stable. Simulations are performed using satellite parameters from the ESEO mission under the European Space Agency's SSETI project. |
Year | DOI | Venue |
|---|---|---|
2009 | 10.1109/TCST.2008.924576 | Control Systems Technology, IEEE Transactions |
Keywords | Field | DocType |
Satellites,Backstepping,Quaternions,Attitude control,Space technology,Feedback,Weight control,Space vehicles,Control systems,Pulse width modulation | Lyapunov function,Control theory,Backstepping,Reaction wheel,Computer science,Control theory,Quaternion,Control engineering,Attitude control,Space exploration,Spacecraft | Journal |
Volume | Issue | ISSN |
17 | 1 | 1063-6536 |
ISBN | Citations | PageRank |
0-7803-9099-7 | 40 | 5.54 |
References | Authors | |
4 | 3 | |
Name | Order | Citations | PageRank |
|---|---|---|---|
| Raymond Kristiansen | 1 | 96 | 16.09 |
| Per Johan Nicklasson | 2 | 129 | 20.47 |
| Jan Tommy Gravdahl | 3 | 327 | 43.60 |