Adaptive, integrated guidance and control design for line-of-sight-based formation flight

Journal of Guidance, Control, and Dynamics

Volumn 30, Issue 5, 2007, Pages 1388-1398

  Kim, Byoung Soo ^a,c,d   Calise, Anthony J ^b,d,e   Sattigeri, Ramachandra J ^b,d,e  

^a Gyeongsang National University   (South Korea)

^b GEORGIA INSTITUTE OF TECHNOLOGY   (United States)

^c Seoul National University   (South Korea)

^d AIAA   (United States)

^e SCHOOL OF AEROSPACE ENGINEERING   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; COMPUTER SIMULATION; FEEDBACK CONTROL; MATHEMATICAL MODELS; NEURAL NETWORKS;

AIRCRAFT ACCELERATION; CONTROL DESIGN; INTEGRATED GUIDANCE; MODELING ERROR;

FLIGHT CONTROL SYSTEMS;

EID: 35348931615     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.27758     Document Type: Article

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