H2 and H∞-optimal gust load alleviation for a flexible aircraft

Proceedings of the American Control Conference

Volumn 3, Issue , 2000, Pages 1872-1876

  Aouf, Nabil ^a   Boulet, Benoit ^a   Botez, Ruxandra ^a  

^a MCGILL UNIVERSITY   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION CONTROL; AERODYNAMIC LOADS; AIRCRAFT; AIRCRAFT MODELS; COMPUTER SIMULATION; FEEDBACK CONTROL; FREQUENCY DOMAIN ANALYSIS; OPTIMAL CONTROL SYSTEMS; TIME DOMAIN ANALYSIS; WHITE NOISE; WIND EFFECTS;

DRYDEN GUST POWER SPECTRAL DENSITY MODEL; GUST LOAD ALLEVIATION; VERTICAL ACCELERATION CONTROL;

CONTROL SYSTEM SYNTHESIS;

EID: 0034540330     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (7)