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A slew and tracking controller sends attitude actuation commands to a set of control moment gyroscopes, and other controllers manage desaturation, detumble, thruster firing, and target acquisition/recovery.
An attitude tracking controller is developed for control moment gyroscope (CMG -actuated satellites, whiCMG -actuatedo achieve accurate attitude tracking in the presatellitesnmodeled external disturbance torques, parametric uncertainty, and nonlinear CMG disturbances.
To maintain space station attitude stable for long-time without frequent control moment gyros (CMGs) saturation interruption, an attitude and momentum management controller in inertial reference is designed.
Why wasn't there a gun control moment before now?
There exists a singularity problem in control moment gyros (CMGs).
Compared with Single Gimbal Control Moment Gyroscopes (SGCMGs), the Variable Speed Control Moment Gyros (VSCMGs) can be easily implemented.
Control Moment Gyros (CMGs) are commonly used as actuators of attitude control in spacecraft.
Accordingly, the control effect is introduced via an equivalent control moment on the circumference.
An adaptive control technique is applied to reorient spacecraft with uncertainty using control moment gyros.
Control moment gyros (CMGs) are widely used as actuators for attitude control in spacecraft.
In this paper a new Attitude Control System is proposed, based on Control Moment Gyroscopes (CMG).
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