Dynamic contraction method approach to robust longitudinal flight control under aircraft parameters variations

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2003, Pages

  Czyba, Roman ^a   Błachuta, Marian J ^a  

^a SILESIAN UNIVERSITY OF TECHNOLOGY   (Poland)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT FLIGHT CONTROLLER; AIRCRAFT PARAMETERS; EXTERNAL DISTURBANCES; FLIGHT PATH ANGLE; INCOMPLETE INFORMATION; LONGITUDINAL MOVEMENTS; NON-STATIONARY OBJECTS; VARYING PARAMETERS;

AIRCRAFT CONTROL; AIRCRAFT MODELS; FIGHTER AIRCRAFT;

AERODYNAMICS;

EID: 84896845813     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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