Torque command steering law for double-gimbaled control moment gyros applied to rotor energy storage
A steering law is presented which has all the features required for space applications, assuming the CMG outer gimbal freedom is unlimited. The reason is the idea of mounting all the outer gimbal axes of the CMGs parallel to each other. This allows the decomposition of the steering law problem into a linear one for the inner gimbal angle rates and a planar one for the outer gimbal angle rates. The inner gimbal angle rates are calculated first, since they are not affected by the outer gimbal angle rates. For the calculation of the outer rates, the inner rates are then known quantities. An outer gimbal angle distribution function (to avoid singularities internal to the total angular momentum envelope) generates distribution rates next, and finally the pseudoinverse method is used to insure that the desired total torque is delivered.
- Research Organization:
- National Aeronautics and Space Administration, Huntsville, AL (USA). George C. Marshall Space Flight Center
- OSTI ID:
- 5631503
- Report Number(s):
- N-85-13879
- Resource Relation:
- Other Information: In NASA, Langley Research Center, an assessment of integrated flywheel system technology, 407-422 p. (N--85-13850 05-20)
- Country of Publication:
- United States
- Language:
- English
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