AbstractA new variable speed control moment gyro (VSCMG) steering law is proposed in order to achieve higher torque precision. The dynamics of VSCMGs is established, and two work modes are then designed according to command torque: control momentum gyro (CMG)/reaction wheel (RW) hybrid mode for the large torque case and RW single mode for the small. When working in the CMG/RW hybrid mode, the steering law deals with the gimbal dead-zone nonlinearity through compensation by RW sub-mode. This is in contrast to the conventional CMG singularity avoidance and wheel speed equalization, as well as the proof of definitely hyperbolic singular property of the CMG sub-mode. When working in the RW single mode, the motion of gimbals will be locked. Both...
Despite the long history of studies on the singularity problem inherent to single-gimbal control mom...
A singularity problem for a single gimbal control moment gyros (SGCMGs) system in a Box configuratio...
A control law for an integrated power/attitude control system (IPACS) for a satellite using variable...
AbstractA new variable speed control moment gyro (VSCMG) steering law is proposed in order to achiev...
A new approach for solving the singularity avoidance problem is presented, based on the observation ...
A new steering law of a pyramid configuration of four control moment gyroscopes (CMGs) is proposed t...
Control moment gyros (CMGs) are spacecraft attitude control actuators which act as torque amplifiers...
141 pagesThis dissertation advances the field of momentum control systems, specifically control mome...
Advances in microelectronics and small satellite engineering have enabled the development of micro C...
In contrast to past studies that have treated the skew angle as fixed in pyramid-type control moment...
This work proposes two algorithms extended from existing steering laws which link conventional contr...
An exact approach for gimbal steering based on generalised-inverse for a cluster of Control Moment G...
Recent practical work in developing combined energy storage and attitude control subsystems for smal...
In this paper, we establish the dynamics of a spacecraft with Variable-Speed Control Moment Gyros (V...
This report investigates and compares steering laws for a control moment gyroscope (CMG) attitude co...
Despite the long history of studies on the singularity problem inherent to single-gimbal control mom...
A singularity problem for a single gimbal control moment gyros (SGCMGs) system in a Box configuratio...
A control law for an integrated power/attitude control system (IPACS) for a satellite using variable...
AbstractA new variable speed control moment gyro (VSCMG) steering law is proposed in order to achiev...
A new approach for solving the singularity avoidance problem is presented, based on the observation ...
A new steering law of a pyramid configuration of four control moment gyroscopes (CMGs) is proposed t...
Control moment gyros (CMGs) are spacecraft attitude control actuators which act as torque amplifiers...
141 pagesThis dissertation advances the field of momentum control systems, specifically control mome...
Advances in microelectronics and small satellite engineering have enabled the development of micro C...
In contrast to past studies that have treated the skew angle as fixed in pyramid-type control moment...
This work proposes two algorithms extended from existing steering laws which link conventional contr...
An exact approach for gimbal steering based on generalised-inverse for a cluster of Control Moment G...
Recent practical work in developing combined energy storage and attitude control subsystems for smal...
In this paper, we establish the dynamics of a spacecraft with Variable-Speed Control Moment Gyros (V...
This report investigates and compares steering laws for a control moment gyroscope (CMG) attitude co...
Despite the long history of studies on the singularity problem inherent to single-gimbal control mom...
A singularity problem for a single gimbal control moment gyros (SGCMGs) system in a Box configuratio...
A control law for an integrated power/attitude control system (IPACS) for a satellite using variable...