Design of Active PWM Control Driver Circuit for Torquer System Using CCII

This research examines a torquer system for satellite attitude control which requires low energy, or average power, to its moment. The magnetic consists of an LR component, source and switching pulse. A mathematical model design equations are presented the torquer. technique using do 3-axis spacecraft has been presented. main goal this is attain specific current in by means CCII action. used since full operation performed high frequency system. closed loop action controller, triangular wave generator, parameters research. scheme's performance considered via analysis simulation model. resulting closed-loop systems robust with respect parametric modeling ambiguity. result attained OrCAD PSPICE, belonging Cadence desired amount value proves efficiency proposed method.