Publication Date:
2016-06-07
Description:
The application of matrix transfer function design techniques to the problem of disturbance rejection on a flexible space structure is demonstrated. The design approach is based on parameterizing a class of stabilizing compensators for the plant and formulating the design specifications as a constrained minimization problem in terms of these parameters. The solution yields a matrix transfer function representation of the compensator. A state space realization of the compensator is constructed to investigate performance and stability on the nominal and perturbed models. The application is made to the ACOSSA (Active Control of Space Structures) optical structure.
Keywords:
SPACECRAFT DESIGN, TESTING AND PERFORMANCE
Type:
JPL Proc. of the Workshop on Identification and Control of Flexible Space Struct., Vol. 3; p 47-62
Format:
application/pdf
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