Application of a modal control design technique to achieve discrete control of distributed parameter systems is considered. Results are presented for application of the design technique to achieve diffraction limited performance from the primary mirror of a space telescope and to provide flutter suppression for an aircraft wing.
Figure control of flexible structures - Optical surfaces of thin deformable primary mirrors
Conference on Decision and Control ; 1980 ; Albuquerque, NM
1980-12-01
Conference paper
No indication
English
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