Piloted sliding mode FTC simulator evaluation for the EL AL flight 1862 incident

AIAA Guidance, Navigation and Control Conference and Exhibit

Volumn , Issue , 2008, Pages

  Alwi, H ^a,c   Edwards, C ^a,c   Stroosma, O ^b,d   Mulder, J A ^b,e  

^a UNIVERSITY OF LEICESTER   (United Kingdom)

^b DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

^c Engineering Department ^*  (Portugal)

^d International Research Institute for Simulation Motion and Navigation   (United States)

^e Faculty of Aerospace Engineering   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AIRCRAFT ACCIDENTS; FLIGHT SIMULATORS; SLIDING MODE CONTROL;

ACTUATOR FAILURES; CLOSED LOOP STABILITY; CONTROL SIGNAL; FAILURE SCENARIOS; FAULT TOLERANT CONTROL; LARGE TRANSPORT AIRCRAFT; MODEL REFERENCE; SLIDING MODES;

CONTROLLERS;

EID: 78651060065     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-7157     Document Type: Conference Paper

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