Satellite Attitude Control by Magnetic Torquers with Variable Magnetic Intensity for Optimization of Power Consumption

M M. Moghaddam; A Salimi

Volume 1, Issue 1 , September 2008, , Pages 37-45

Abstract
  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 an ...  Read More