Name
Title | ||
|---|---|---|
A Simple Velocity-Free Controller for Attitude Regulation of a Spacecraft With Delayed Feedback |
Abstract | ||
|---|---|---|
In this note, we consider the application of a velocity-free controller for attitude regulation of a rigid spacecraft with gas jet actuators when the effects of time-delays in the feedback loop are taken into consideration. Simple sufficient conditions for exponential stability are presented. Some structural properties of the resulting closed-loop system are studied, and relevant design tools are demonstrated. |
Year | DOI | Venue |
|---|---|---|
2004 | 10.1109/TAC.2003.821406 | IEEE Trans. Automat. Contr. |
Keywords | Field | DocType |
Velocity control,Attitude control,Space vehicles,Delay effects,Stability,Angular velocity,Feedback loop,Velocity measurement,Angular velocity control,Sufficient conditions | Control theory,Control theory,Feedback loop,Control engineering,Attitude control,Exponential stability,Mathematics,Actuator,Spacecraft | Journal |
Volume | Issue | ISSN |
49 | 1 | 0018-9286 |
Citations | PageRank | References |
12 | 1.02 | 4 |
Authors | ||
3 | ||
Name | Order | Citations | PageRank |
|---|---|---|---|
| Amit Ailon | 1 | 91 | 15.23 |
| R. Segev | 2 | 12 | 1.02 |
| S. Arogeti | 3 | 15 | 1.78 |