Automatic landing system design using feedback linearization method

Collection of Technical Papers - 2007 AIAA InfoTech at Aerospace Conference

Volumn 1, Issue , 2007, Pages 230-249

  Biju Prasad, B ^a   Pradeep, S ^b  

^a INDIAN SPACE RESEARCH ORGANISATION   (India)

^b INDIAN INSTITUTE OF SCIENCE   (India)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; FEEDBACK LINEARIZATION; FIGHTER AIRCRAFT; GROUND EFFECT; NONLINEAR CONTROL SYSTEMS; WIND TUNNELS;

AUTOMATIC LANDING SYSTEM DESIGN; ELEVATOR DYNAMICS; THREE-DEGREE-OF-FREEDOM NONLINEAR AIRCRAFT MODEL; THROTTLE CONTROLS;

AIRCRAFT LANDING SYSTEMS;

EID: 35648983476     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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