A steering law for three double-gimbal control moment gyro systems
Abstract
A steering law for three double-gimbal control moment gyro (CMG) systems is proposed. This steering law is applicable to systems with almost any configuration of CMGs and the CMG-out operation needs no special modification. Examples of three double gimbal CMG systems in an orthogonal configuration and in a parallel configuration are shown along with the results of digital simulations. Simulation results show that any command torque can always be met except when the system is in a singular state and that, whenever the system is in, or close to, a singularity, the steering law drives the system state out of the vicinity of the singularity.
- Publication:
-
NASA STI/Recon Technical Report N
- Pub Date:
- March 1975
- Bibcode:
- 1975STIN...7523925Y
- Keywords:
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- Control Moment Gyroscopes;
- Gimbals;
- Steering;
- Aerodynamic Configurations;
- Digital Simulation;
- Problem Solving;
- Torque;
- Instrumentation and Photography