Autopilot design for highly maneuvering STT missiles via singular perturbation-like technique

IEEE Transactions on Control Systems Technology

Volumn 7, Issue 5, 1999, Pages 527-541

  Lee, Ju Il ^b   Ha, In Joong ^a,b  

^a IEEE

^b Seoul National University   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; CONTROL NONLINEARITIES; FEEDBACK; LINEARIZATION; MISSILES; PERTURBATION TECHNIQUES;

FEEDBACK-LINEARIZATION TECHNIQUES; SKID-TO-TURN (STT) MISSILES;

TRACKING (POSITION);

EID: 0032646897     PISSN: 10636536     EISSN: None     Source Type: Journal    
DOI: 10.1109/87.784417     Document Type: Article

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