Aeroservoelastic interaction between aircraft structural and control design schemes

Journal of Guidance, Control, and Dynamics

Volumn 22, Issue 4, 1999, Pages 513-519

  Idan, Moshe ^a   Karpel, Mordechay ^a   Moulin, Boris ^a  

^a TECHNION ISRAEL INSTITUTE OF TECHNOLOGY   (Israel)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT PARTS AND EQUIPMENT; APPROXIMATION THEORY; LINEAR CONTROL SYSTEMS; MATHEMATICAL MODELS; MATRIX ALGEBRA; OPTIMIZATION; SENSITIVITY ANALYSIS; SOFTWARE ENGINEERING; STATE SPACE METHODS; SYSTEM STABILITY;

AEROSERVOELASTIC LOOP; AIRCRAFT STRUCTURAL DESIGN; LINEAR CONTROL LAWS; UNSTEADY FORCE COEFFICIENT;

CONTROL SYSTEM SYNTHESIS;

EID: 0032629010     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4427     Document Type: Article

References (12)

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