Sliding mode and inertial delay control based missile guidance

IEEE Transactions on Aerospace and Electronic Systems

Volumn 48, Issue 4, 2012, Pages 3331-3346

  Phadke, S B ^a   Talole, S E ^a  

^a Department of Instrumentation & Control Engineering   (India)

Author keywords

[No Author keywords available]

Indexed keywords

CLOSED LOOP STABILITY; DELAY CONTROL; GUIDANCE LAWS; GUIDANCE LOOPS; PROPORTIONAL NAVIGATION GUIDANCE; SLIDING MODES; TARGET ACCELERATION;

MISSILES;

ELECTRONIC GUIDANCE SYSTEMS;

EID: 84867535241     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/TAES.2012.6324711     Document Type: Article

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