Uncertainty modelling for the control of an active structureTwo approaches to uncertainty modeling of a precision active truss structure for control design are presented. The first approach is based on the H(infinity) optimal control theory, which is used for robust control design with an additive uncertainty model. It is designed to provide vibration suppression to selected modes of the structure at the accelerometer locations. The uncertainty model can be used as an adjustable design parameter which will enable a study of the trade-offs between performance and robust stability. The second approach is based on mu-synthesis. Although the structured singular value can be used to analyze the robustness of any type of uncertainty, there exist difficulties in synthesis if the uncertainty block contains both real and complex variations. Mu-synthesis techniques do not allow for real-parameter variations in the synthesis procedure. The use of a complex variation description enclosing the real variation is suggested.
Document ID
19910054207
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Blackwood, G. H. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Chu, C.-C. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Fanson, J. L. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)