Name
Abstract | ||
|---|---|---|
In this paper, we utilize the roll momentum bias to control the pitch/yaw attitude of the satellite. While the previous control approaches have used the PD control approach, we design a new PID controller in order to improve the transient response over the existing methods. Through the example, we show that our control approach indeed improves the control performance over the existing results. For simulation, the system parameters are taken from the values of KOREASAT1. |
Year | DOI | Venue |
|---|---|---|
2013 | 10.1109/ASCC.2013.6606154 | ASCC |
Keywords | Field | DocType |
pd control,aerospace control,control system synthesis,momentum,position control,space vehicles,three-term control,transient response,koreasat1,pd control approach,pid controller,pitch-yaw momentum position control approach,roll momentum bias,roll momentum biased satellite system,coarse sun sensor,feedback controller,momentum biased satellite,reaction wheel,yaw/pitch control,torque,attitude control,satellites | Transient response,Satellite,PID controller,Control theory,Satellite system,Control engineering,Momentum,Engineering,Control moment gyroscope | Conference |
ISSN | ISBN | Citations |
2072-5639 | 978-1-4673-5767-8 | 0 |
PageRank | References | Authors |
0.34 | 0 | 2 |
Name | Order | Citations | PageRank |
|---|---|---|---|
| Kyung-Hyun Oh | 1 | 0 | 0.34 |
| Hae-Yeong Gwon | 2 | 0 | 0.34 |