Satellite Attitude Control by Magnetic Torquers with Variable Magnetic Intensity for Optimization of Power Consumption
This Paper presents a dynamic model of a micro-satellite in Mesbah class. At this model aerodynamic torque and solar radiation pressure torques are considered as disturbance torques. Gravity gradient torque is assumed as stabilizing torque and acts as a passive controller. Magnetic torquers act as a...
| Main Authors: | , |
|---|---|
| Format: | Article |
| Language: | fas |
| Published: |
Aerospace Research Institute
2008-04-01
|
| Series: | فصلنامه علوم و فناوری فضایی |
| Subjects: | |
| Online Access: | https://jsst.ias.ir/article_14359_7c1062c2cb6d95c22d3937d16ff3a076.pdf |