Problem of precision missile guidance: LQR and H∞ control frameworks

IEEE Transactions on Aerospace and Electronic Systems

Volumn 39, Issue 3, 2003, Pages 901-910

  Savkin, Andrey V ^a   Pathirana, Pubudu N ^b   Faruqi, Farhan A ^c  

^a UNIVERSITY OF NEW SOUTH WALES   (Australia)

^b DEAKIN UNIVERSITY   (Australia)

^c DEFENCE SCIENCE AND TECHNOLOGY ORGANISATION   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL THEORY; FEEDBACK CONTROL; KINEMATICS; LINEAR CONTROL SYSTEMS; OPTIMAL CONTROL SYSTEMS;

MISSILE BODY ALTITUDE; PRECISION MISSILE GUIDANCE;

ELECTRONIC GUIDANCE SYSTEMS;

EID: 0345566280     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/TAES.2003.1238744     Document Type: Article

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