Guidance and control of missile interceptor using second-order sliding modes

IEEE Transactions on Aerospace and Electronic Systems

Volumn 45, Issue 1, 2009, Pages 110-124

  Shtessel, Yuri B ^a   Shkolnikov, Ilya A ^b   Levant, Arie ^c  

^a UNIVERSITY OF ALABAMA IN HUNTSVILLE   (United States)

^b Z/I Imaging Corporation   (United States)

^c TEL AVIV UNIVERSITY   (Israel)

Author keywords

Acceleration; Accuracy; Aerodynamics; Kinematics; Missiles; Observers; Robustness

Indexed keywords

ACCURACY; CONTROL SYSTEM PERFORMANCE; GUIDANCE AND CONTROLS; HYPERVELOCITY; MISSILE INTERCEPTORS; OBSERVERS; PLANAR MODELS; ROBUSTNESS; SECOND-ORDER SLIDING MODE CONTROLS; SECOND-ORDER SLIDING MODES; TARGET APPLICATIONS;

AERODYNAMICS; CONTROL SYSTEM ANALYSIS; KINEMATICS; MISSILES; OBSERVABILITY; ROBUSTNESS (CONTROL SYSTEMS);

FLIGHT CONTROL SYSTEMS;

EID: 65449152927     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/TAES.2009.4805267     Document Type: Article

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