Fundamental aeroservoelastic study combining unsteady computational fluid mechanics with adaptive control

Journal of Guidance, Control, and Dynamics

Volumn 23, Issue 6, 2000, Pages 1117-1126

  Guillot, Damien M ^a,b   Friedmann, Peretz P ^a,c  

^a UNIVERSITY OF CALIFORNIA   (United States)

^b Mech and Aerosp Eng Department   (France)

^c UNIVERSITY OF MICHIGAN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; ADAPTIVE CONTROL SYSTEMS; AIRFOILS; CLOSED LOOP CONTROL SYSTEMS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; DEGREES OF FREEDOM (MECHANICS); DIGITAL CONTROL SYSTEMS; FLUTTER (AERODYNAMICS); SHOCK WAVES;

AEROSERVOELASTIC; FLUTTER SUPPRESSION; NONLINEAR TRANSONIC AEROELASTIC;

TRANSONIC AERODYNAMICS;

EID: 0034318042     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4663     Document Type: Article

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