Hybrid adaptive flight control with bounded linear stability analysis

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference 2007

Volumn 2, Issue , 2007, Pages 1117-1138

  Nguyen, Nhan T ^a,c,d   Bakhtiari Nejad, Maryam ^a,c,d   Huang, Yong ^b,e  

^a NASA AMES RESEARCH CENTER   (United States)

^b CLEMSON UNIVERSITY   (United States)

^c Intelligent Systems Division   (United States)

^d AIAA   (United States)

^e Clemson University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDED LINEAR STABILITY ANALYSIS; DIRECT ADAPTIVE LAW; DYNAMIC INVERSION CONTROL MODEL; HYBRID ADAPTIVE CONTROL METHOD;

ADAPTIVE CONTROL SYSTEMS; ESTIMATION; LEAST SQUARES APPROXIMATIONS; LINEAR STABILITY ANALYSIS; LYAPUNOV FUNCTIONS; NEURAL NETWORKS; TRACKING (POSITION);

FLIGHT CONTROL SYSTEMS;

EID: 37249028163     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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