Design of optimal midcourse guidance sliding-mode control for missiles with TVC

IEEE Transactions on Aerospace and Electronic Systems

Volumn 39, Issue 3, 2003, Pages 824-837

  Yeh, Fu Kuang ^a   Chien, Hsiuan Hau ^b   Fu, Li Chen ^a  

^a NATIONAL TAIWAN UNIVERSITY   (Taiwan)

^b ALi Corporation   (Taiwan)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION; AERODYNAMICS; BALLISTICS; CONTROL SYSTEM SYNTHESIS; DEGREES OF FREEDOM (MECHANICS); LYAPUNOV METHODS; MISSILES; SLIDING MODE CONTROL; SYSTEM STABILITY;

AUTOPILOT SYSTEM; NONLINEAR MIDCOURSE MISSILE CONTROLLER; THRUST VECTOR CONTROL;

ELECTRONIC GUIDANCE SYSTEMS;

EID: 0344272295     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/TAES.2003.1238739     Document Type: Article

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