Satellite 3Axis Attitude Control Using the Combination of Reaction Wheels and Thrusters
In this paper, the combination of reaction wheels and thrusters is applied to attitude control of a satellite. First, governing equations of satellite attitude dynamics are given using quaternion and PID controller is designed based on the satellite quaternion to determine the applied control torque...
| Main Authors: | , , |
|---|---|
| Format: | Article |
| Language: | fas |
| Published: |
Aerospace Research Institute
2018-11-01
|
| Series: | فصلنامه علوم و فناوری فضایی |
| Subjects: | |
| Online Access: | https://jsst.ias.ir/article_81073_93726b02415201240c81ce9c47304202.pdf |