Stability augmentation for crosswind landings using Dynamic Cell Structures

AIAA Guidance, Navigation and Control Conference and Exhibit

Volumn , Issue , 2008, Pages

  Sivakumar, Achudhan ^a   Phang, Tze Seng ^a   Tan, Colin Keng Yan ^a  

^a NATIONAL UNIVERSITY OF SINGAPORE   (Singapore)

Author keywords

[No Author keywords available]

Indexed keywords

CELL STRUCTURE; CENTERLINES; COMPLEX COMPUTATION; CONTROL SURFACE DEFLECTION; CONVERGENCE TIME; GAIN CONTROLLERS; HIGH PERFORMANCE SYSTEMS; HYBRID CONTROL SYSTEMS; INPUT SPACE; LATERAL STABILITY; NONLINEAR DYNAMIC INVERSION; OFF-LINE LEARNING; PROPORTIONAL INTEGRAL DERIVATIVES; REAL TIME; X-PLANE;

AIRCRAFT; AIRCRAFT CONTROL; COMPUTATIONAL COMPLEXITY; CONTROL SURFACES; CONTROL THEORY; DISTRIBUTED PARAMETER NETWORKS; FLIGHT CONTROL SYSTEMS; FLIGHT DYNAMICS; IDENTIFICATION (CONTROL SYSTEMS); LANDING; LEARNING ALGORITHMS; NAVIGATION; PROPORTIONAL CONTROL SYSTEMS; REMOTE CONTROL; SYSTEM STABILITY; THREE TERM CONTROL SYSTEMS; TWO TERM CONTROL SYSTEMS;

CONTROL SYSTEM STABILITY;

EID: 78651059815     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (16)

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