Inner loop control of supersonic aircraft in the presence of aeroelastic modes

IEEE Transactions on Control Systems Technology

Volumn 6, Issue 6, 1998, Pages 730-739

  Joshi, Suresh M ^a,c   Kelkar, Atul G ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b KANSAS STATE UNIVERSITY   (United States)

^c IEEE   (United States)

Author keywords

Aeroelastic mode control; Aircraft control; Linear quadratic control; Robust control; Robustness; Supersonic aircraft

Indexed keywords

CONTROL SYSTEM SYNTHESIS; FLEXIBLE STRUCTURES; FREQUENCY DOMAIN ANALYSIS; LYAPUNOV METHODS; MATHEMATICAL MODELS; ROBUSTNESS (CONTROL SYSTEMS); SUPERSONIC AERODYNAMICS; SUPERSONIC AIRCRAFT; SYSTEM STABILITY; TIME DOMAIN ANALYSIS; UNCERTAIN SYSTEMS;

AEROELASTIC MODE CONTROL; LINEAR-QUADRATIC CONTROL; LONGITUDINAL CONTROL SYSTEMS;

LINEAR CONTROL SYSTEMS;

EID: 0032204981     PISSN: 10636536     EISSN: None     Source Type: Journal    
DOI: 10.1109/87.726534     Document Type: Article

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