Robust flight controller design that takes into account handling quality

Journal of Guidance, Control, and Dynamics

Volumn 28, Issue 1, 2005, Pages 71-77

  Tokutake, Hiroshi ^a,d   Sato, Masayuki ^b,e   Satoh, Atsushi ^c,f  

^a Osaka Prefecture University   (Japan)

^b JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^c NARA INSTITUTE OF SCIENCE AND TECHNOLOGY   (Japan)

^d Department of Aerospace Engineering ^*  (Japan)

^e Institute of Space Technology and Aeronautics   (Japan)

^f Nara Institute of Science and Technology   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION; EIGENVALUES AND EIGENFUNCTIONS; ERROR ANALYSIS; MATRIX ALGEBRA; ROBUSTNESS (CONTROL SYSTEMS); SYSTEMS ANALYSIS;

CONTROL-ANTICIPATION-PARAMETER (CAP); DIRECT-LIFT-CONTROL (DLC) ANGLE; FLIGHT CONTROLLER DESIGN; GRADIENT COMPONENT;

FLIGHT DYNAMICS;

EID: 12744279671     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.6405     Document Type: Article

References (14)

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