An analytical sensitivity method for use in integrated aeroservoelastic aircraft design

DOI10.1016/0888-3270(90)90016-EzbMath0709.73054OpenAlexW2032881694MaRDI QIDQ3493591

Michael G. Gilbert

Publication date: 1990

Published in: Mechanical Systems and Signal Processing (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0888-3270(90)90016-e

zbMATH Keywords

changes in fixed design integration parameterscontrolled system responsesdesign sensitivity analysis methodhierarchical design methodologylinear quadratic Gaussian (LQG) optimal control lawswing bending natural frequency

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Control, switches and devices (``smart materials) in solid mechanics (74M05) Vibrations in dynamical problems in solid mechanics (74H45) Optimization problems in solid mechanics (74P99)

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