Nonlinear autopilot and guidance for a highly maneuverable missile

Proceedings of the American Control Conference

Volumn 2, Issue , 1994, Pages 2293-2297

  Lian, Kuang Yow ^a   Fu, Li Chen ^a   Chuang, Dung Ming ^a   Kuo, Teh Son ^a  

^a CHUNG YUAN CHRISTIAN UNIVERSITY   (Taiwan)

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATION THEORY; AUTOMATION; COMPUTER SIMULATION; CONTROL EQUIPMENT; CONTROL THEORY; ELECTRONIC GUIDANCE SYSTEMS; MISSILES; ROBUSTNESS (CONTROL SYSTEMS);

AERIAL ENGAGEMENT SCENARIO; AUTOPILOT; BANK TO TURN TERMINAL HOMING MISSILES; DIFFERENTIAL GEOMETRIC CONTROL THEORY; NONLINEAR CONTROL THEORY;

NONLINEAR CONTROL SYSTEMS;

EID: 0028572282     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (21)