Flight envelope expansion in landing phase using classic, intelligent, and adaptive controllers

Journal of Aircraft

Volumn 43, Issue 1, 2006, Pages 91-101

  Malaek, S M B ^a,c   Izadi, Hojjat A ^a,c   Pakmehr, Mehrdad ^b,d,e  

^a SHARIF UNIVERSITY OF TECHNOLOGY   (Iran)

^b Civil and Environmental Engineering   (Canada)

^c Aerospace Engineering Department   (Iran)

^d Mechanical and Industrial Engineering Department   (Canada)

^e AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; AIRCRAFT; AIRCRAFT LANDING; CONTROL EQUIPMENT; INTELLIGENT CONTROL; LEARNING SYSTEMS; NEURAL NETWORKS; TURBULENCE;

FLIGHT ENVELOPE EXPANSION; FUNCTIONAL ARCHITECTURE; LEARNING CAPABLE CONTROL SYSTEM (LCCS);

FLIGHT DYNAMICS;

EID: 33644619443     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.13197     Document Type: Article

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