Enhanced eigenstructure assignment for aeroelastic control application

Aerospace Science and Technology

Volumn 8, Issue 6, 2004, Pages 533-543

  Merkel, Maximilian ^a   Gojny, Marcus Heinrich ^a   Carl, Udo B ^a  

^a HAMBURG UNIVERSITY OF TECHNOLOGY   (Germany)

Author keywords

Aeroservoelasticity; Damping augmentation; Eigenstructure assignment; Flexible aircraft; Flutter margin; Hardware in the loop simulation; Robust controller design; Structural vibrations

Indexed keywords

COMPUTER SIMULATION; DAMPING; EIGENVALUES AND EIGENFUNCTIONS; FEEDBACK CONTROL; MATHEMATICAL MODELS; OPTIMIZATION; PROBLEM SOLVING; ROBUSTNESS (CONTROL SYSTEMS); STABILIZATION;

AEROSERVOELASTICITY; DAMPING AUGMENTATION; EIGENSTRUCTURE ASSIGNMENT; FLEXIBLE AIRCRAFTS; HARDWARE-IN-THE-LOOP SIMULATION; ROBUST CONTROLLER DESIGN; STRUCTURAL VIBRATIONS;

AERODYNAMICS;

EID: 4243201400     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2004.06.001     Document Type: Article

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