Empirical Virtual Sliding Target Guidance Law Design: An Aerodynamic Approach

IEEE Transactions on Aerospace and Electronic Systems

Volumn 39, Issue 4, 2003, Pages 1179-1190

  Raju, P A ^b   Ghose, Debasish ^a  

^a INDIAN INSTITUTE OF SCIENCE   (India)

^b TATA CONSULTANCY SERVICES   (India)

Author keywords

[No Author keywords available]

Indexed keywords

SINGLE PERTURBATION GUIDANCE LAW; VIRTUAL SLIDING TARGET (VST) GUIDANCE LAW;

COMPUTER SIMULATION; DEGREES OF FREEDOM (MECHANICS); KINEMATICS; MATHEMATICAL MODELS; MISSILES; OPTIMAL CONTROL SYSTEMS; OPTIMIZATION; TRAJECTORIES;

AERODYNAMICS;

EID: 1642271440     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/TAES.2003.1261120     Document Type: Article

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