Geometric analysis of flight control command for tactical missile guidance

IEEE Transactions on Control Systems Technology

Volumn 9, Issue 2, 2001, Pages 234-243

  Kuo, Chen Yuan ^a   Soetanto, Didik ^a   Chiou, Ying Chwan ^b  

^a Arizona State University   (United States)

^b AEROSPACE INDUSTRIAL DEVELOPMENT CORPORATION   (Taiwan)

Author keywords

Curvature command; Differential geometry; Engagement geometry; Flight control; Frenet Serret formula; Miss condition; Missile guidance; Target capture

Indexed keywords

COMPUTATIONAL GEOMETRY; CURVE FITTING; DIFFERENTIAL EQUATIONS; ELECTRONIC GUIDANCE SYSTEMS; NONLINEAR EQUATIONS; SYSTEM STABILITY; VELOCITY CONTROL;

CURVATURE COMMAND; DIFFERENTIAL GEOMETRY; ENGAGEMENT GEOMETRY; FLIGHT CONTROL COMMAND; FRENET-SERRET FORMULA; GEOMETRIC CURVE THEORY; TACTICAL MISSILE GUIDANCE; VELOCITY VECTORS;

CONTROL SYSTEM ANALYSIS;

EID: 0035271688     PISSN: 10636536     EISSN: None     Source Type: Journal    
DOI: 10.1109/87.911375     Document Type: Article

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