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Reduced-Order Optimal Feedback Control Law Synthesis for Fl..:
Mukhopadhyay, V.
;
Newsom, J.R.
;
Abel, I.
Journal of Guidance, Control, and Dynamics. 5 (1982) 4 - p. 389-395 , 1982
Link:
https://doi.org/10.2514/3.56187
RT Journal T1 <Title>Reduced-Order Optimal Feedback Control Law Synthesis for Flutter Suppression</Title> UL https://suche.suub.uni-bremen.de/peid=cr-10.2514_3.56187&Exemplar=1&LAN=DE A1 Mukhopadhyay, V. A1 Newsom, J.R. A1 Abel, I. PB American Institute of Aeronautics and Astronautics (AIAA) YR 1982 SN 0731-5090 SN 1533-3884 JF Journal of Guidance, Control, and Dynamics VO 5 IS 4 SP 389 OP 395 LK http://dx.doi.org/https://doi.org/10.2514/3.56187 DO https://doi.org/10.2514/3.56187 SF ELIB - SuUB Bremen
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