New parametric affine modeling and control for skid-to-turn missiles

IEEE Transactions on Control Systems Technology

Volumn 9, Issue 2, 2001, Pages 335-347

  Chwa, Dongkyoung ^b   Choi, Jin Young ^a,b  

^a Seoul National University ^*

^b Seoul National University   (South Korea)

Author keywords

Aerodynamic coefficient in closed form; Feedback linearizing controller; Function approximation; Parametric affine missile model; Skid to turn (STT) missiles

Indexed keywords

ACOUSTIC WAVE VELOCITY; AERODYNAMICS; APPROXIMATION THEORY; AUTOMATIC PILOTS; CLOSED LOOP CONTROL SYSTEMS; CURVE FITTING; FEEDBACK CONTROL; MATHEMATICAL MODELS; MISSILES; SYSTEM STABILITY; TABLE LOOKUP;

AERODYNAMIC COEFFICIENTS; FEEDBACK LINEARIZING CONTROLLER; FUNCTION APPROXIMATION TECHNIQUE; MACH NUMBER; PARAMETRIC AFFINE MISSILE MODEL; SKID-TO-TURN MISSILES;

ACCELERATION CONTROL;

EID: 0035271797     PISSN: 10636536     EISSN: None     Source Type: Journal    
DOI: 10.1109/87.911385     Document Type: Article

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