Robust H2 design for lateral flight control of highly flexible aircraft

Journal of Guidance, Control, and Dynamics

Volumn 25, Issue 3, 2002, Pages 502-510

  Alazard, Daniel ^a  

^a ONERA   (France)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; AIRCRAFT INSTRUMENTS; AIRCRAFT MOCKUPS; DEGREES OF FREEDOM (MECHANICS); FEEDBACK; FREQUENCY DOMAIN ANALYSIS; MODAL ANALYSIS; NONLINEAR CONTROL SYSTEMS; NUMERICAL METHODS; ROBUSTNESS (CONTROL SYSTEMS); STABILITY; TIME DOMAIN ANALYSIS;

DYNAMIC OUTPUT FEEDBACK SATISFYING MODEL SPECIFICATIONS; EIGENSTRUCTURE ASSIGNMENT; FLEXIBLE AIRCRAFT; FREQUENCY DOMAIN SYNTHESIS; LATERAL FLIGHT CONTROL DESIGN; LINEAR QUADRATIC GAUSSIAN COMPENSATOR; PARAMETRIC ROBUSTNESS DESIGN; TWO INPUT TWO OUTPUT PROBLEM FORMALISM;

CONTROL SYSTEM SYNTHESIS;

EID: 0036564348     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4910     Document Type: Article

References (19)

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