Analysis of aircraft pitch axis stability augmentation system using sum of squares optimization

Proceedings of the American Control Conference

Volumn 3, Issue , 2005, Pages 1497-1502

  Krishnaswamy, Kailash ^a   Papageorgiou, George ^a   Glavaski, Sonja ^a   Papachristodoulou, Antonis ^b  

^a HONEYWELL TECHNOLOGY CENTER   (United States)

^b CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT PITCH AXIS; DYNAMIC INVERSION; NONLINEAR MODELS; SUM OF SQUARES (SOS);

AIRCRAFT MODELS; CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; FLIGHT DYNAMICS; MATHEMATICAL MODELS; NONLINEAR SYSTEMS; SYSTEM STABILITY;

AIRCRAFT;

EID: 23944497181     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

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