Despite the long history of studies on the singularity problem inherent to single-gimbal control moment gyroscopes, few existing gimbal steering laws can both accurately track moments and escape or avoid every type of singularity. The most-referenced steering laws perturb the system suboptimally at every singularity to enforce escape, which creates a tradeoff between minimizing escape time and minimizing transient tracking errors and gimbal rates. It is shown that no such tradeoff is necessary by proposing new singularity measures to quantify the current and future reference moment tracking capabilities and defining explicitly how an anticipated singularity can be avoided or escaped. Using these measures to separate and prioritize the tasks...
In the field of momentum exchange attitude control systems, single gimbal control moment gyros (SGCM...
PatentA method is described for avoiding gyrocopic singularities during attitude correction to a syt...
Control Moment Gyroscope (CMG) is an effective candidate for agile satellites and large spacecraft a...
Despite the long history of studies on the singularity problem inherent to single-gimbal control mom...
A new approach for solving the singularity avoidance problem is presented, based on the observation ...
In this thesis, the kinematic properties of Single Gimballed Control Moment Gyroscopes (SGCMGs) are ...
Geometric singularity problems are principle difficulties of single-gimbal control moment gyros in s...
Abstract: Problem statement: A cluster of small-sized Single-Gimbal Control Moment Gyros (SGCMGs) is...
A singularity problem for a single gimbal control moment gyros (SGCMGs) system in a Box configuratio...
Gyroscopic actuation is appealing for wearable applications due to its ability to impart free moment...
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...
This paper addresses the problem of singularity avoidance in a cluster of four Single-Gimbal Control...
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...
In the field of momentum exchange attitude control systems, single gimbal control moment gyros (SGCM...
PatentA method is described for avoiding gyrocopic singularities during attitude correction to a syt...
Control Moment Gyroscope (CMG) is an effective candidate for agile satellites and large spacecraft a...
Despite the long history of studies on the singularity problem inherent to single-gimbal control mom...
A new approach for solving the singularity avoidance problem is presented, based on the observation ...
In this thesis, the kinematic properties of Single Gimballed Control Moment Gyroscopes (SGCMGs) are ...
Geometric singularity problems are principle difficulties of single-gimbal control moment gyros in s...
Abstract: Problem statement: A cluster of small-sized Single-Gimbal Control Moment Gyros (SGCMGs) is...
A singularity problem for a single gimbal control moment gyros (SGCMGs) system in a Box configuratio...
Gyroscopic actuation is appealing for wearable applications due to its ability to impart free moment...
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...
This paper addresses the problem of singularity avoidance in a cluster of four Single-Gimbal Control...
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...
In the field of momentum exchange attitude control systems, single gimbal control moment gyros (SGCM...
PatentA method is described for avoiding gyrocopic singularities during attitude correction to a syt...
Control Moment Gyroscope (CMG) is an effective candidate for agile satellites and large spacecraft a...