Adaptive robust bank-to-turn missile autopilot design using neural networks

Journal of Guidance, Control, and Dynamics

Volumn 20, Issue 2, 1997, Pages 346-354

  Fu, Li Chen ^a   Chang, Wei Der ^a   Yang, Jung Hua ^a   Kuo, Te Son ^a  

^a NATIONAL TAIWAN UNIVERSITY   (Taiwan)

Author keywords

[No Author keywords available]

Indexed keywords

CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; CONTROL THEORY; CONVERGENCE OF NUMERICAL METHODS; ERRORS; FEEDFORWARD NEURAL NETWORKS; LYAPUNOV METHODS; MISSILES; PERFORMANCE; ROBUSTNESS (CONTROL SYSTEMS);

CLOSED LOOP SYSTEM; OPTIMAL NEURAL NETWORKS; ROBUST ADAPTIVE CONTROL THEORY;

ADAPTIVE CONTROL SYSTEMS;

EID: 0031103518     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4044     Document Type: Article

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