Add to ORKGIn case two control moment gyros fail, attitude control of Skylab can be maintained with the thruste...
Single-Gimbal Control Moment Gyro (SGCMG) systems have been investigated for attitude control of the...
The development of a prototype Control Moment Gyroscope (CMG) is discussed. Physical characteristics...
In the field of momentum exchange attitude control systems, single gimbal control moment gyros (SGCM...
Mounting of double-gimbaled control moment gyros (CMG's) of unlimited outer gimbal angle freedom wit...
Parallel mounting of double-gimbaled control moment gyros (DG CMG) is discussed in terms of simplifi...
Twin gyro coupling system with compensation and nonlinear control for satellite attitude stabilizati...
Angular momentum vector distribution and rotation laws for three double-gimbaled control moment gyro
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1998.Includes...
Feasibility of using single three-gimbaled control moment gyro for control of orbital spacecraft mod...
This paper presents an approach for controlling spacecraft equipped with control moment gyroscopes. ...
Four 4760 Nms (3510 ft-lbf-s) Double Gimbal Control Moment Gyroscopes (DGCMG) with unlimited gimbal ...
This paper describes an application of nonlinear controllability theory to the problem of spacecraft...
This paper considers control strategies for maneuvering spacecraft using Single-Gimbal Control Momen...
Control moment gyros are common spacecraft attitude control devices that can be mounted at different...
In case two control moment gyros fail, attitude control of Skylab can be maintained with the thruste...
Single-Gimbal Control Moment Gyro (SGCMG) systems have been investigated for attitude control of the...
The development of a prototype Control Moment Gyroscope (CMG) is discussed. Physical characteristics...
In the field of momentum exchange attitude control systems, single gimbal control moment gyros (SGCM...
Mounting of double-gimbaled control moment gyros (CMG's) of unlimited outer gimbal angle freedom wit...
Parallel mounting of double-gimbaled control moment gyros (DG CMG) is discussed in terms of simplifi...
Twin gyro coupling system with compensation and nonlinear control for satellite attitude stabilizati...
Angular momentum vector distribution and rotation laws for three double-gimbaled control moment gyro
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1998.Includes...
Feasibility of using single three-gimbaled control moment gyro for control of orbital spacecraft mod...
This paper presents an approach for controlling spacecraft equipped with control moment gyroscopes. ...
Four 4760 Nms (3510 ft-lbf-s) Double Gimbal Control Moment Gyroscopes (DGCMG) with unlimited gimbal ...
This paper describes an application of nonlinear controllability theory to the problem of spacecraft...
This paper considers control strategies for maneuvering spacecraft using Single-Gimbal Control Momen...
Control moment gyros are common spacecraft attitude control devices that can be mounted at different...
In case two control moment gyros fail, attitude control of Skylab can be maintained with the thruste...
Single-Gimbal Control Moment Gyro (SGCMG) systems have been investigated for attitude control of the...
The development of a prototype Control Moment Gyroscope (CMG) is discussed. Physical characteristics...