the rotor axis to generate an output torque a control system has a sensor for determining the output torque and a processor in communication with the rotor assembly the gimbal assembly and the sensor the processor requests the target torque and establishes a feedback control loop to generate a torque error signal based on the output torque for bringing the output torque within a predetermined range of the target torque application_number US 14846708 A description the present invention overcomes many of the prior art problems associated with control moment gyroscopes the advantages and other features of the control moment gyroscopes disclosed herein will become more readily apparent to those having ordinary skill in the art from the following detailed description of certain embodiments taken in conjunction with the drawings which set forth representative embodiments of the present invention and wherein like reference numerals identify similar structural elements unless otherwise specified the illustrated embodiments can be understood as providing exemplary features of varying detail of certain embodiments and therefore unless otherwise specified features components modules elements and or aspects of the illustrations can be otherwise combined interconnected sequenced separated interchanged positioned and or rearranged without materially departing from the disclosed systems or methods additionally the shapes and sizes of components are also exemplary and unless otherwise specified can be altered without materially affecting or limiting the disclosed technology referring to fig1 a schematic view of a system 10 with a control moment gyroscope cmg 20 configured for use with a direct torque actuator control system dtacs 30 is shown the dtacs 30 includes.