Flexible aircraft model identification for control law design

DOI10.1016/S1270-9638(02)01197-5zbMath1023.93023MaRDI QIDQ4418875

A. Bucharles, Pierre Vacher

Publication date: 30 July 2003

Published in: Aerospace Science and Technology (Search for Journal in Brave)

zbMATH Keywords

designoutput error minimizationeigensystem realization algorithmflexible aircraftERA algorithmrigid and elastic modes

Mathematics Subject Classification ID

System identification (93B30) Application models in control theory (93C95) Design techniques (robust design, computer-aided design, etc.) (93B51)

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