Adaptive control for feedback-linearized missiles with uncertainties

IEEE Transactions on Aerospace and Electronic Systems

Volumn 36, Issue 2, 2000, Pages 467-481

  Choi, Jin Young ^a,d   Chwa, Dongkyoung ^b,d   Kim, Min Soo ^c  

^a Seoul National University ^*

^b Seoul National University   (South Korea)

^c Daewoo Electronics Co   (South Korea)

^d Department of Aerospace Engineering   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; AERODYNAMICS; COMPUTER SIMULATION; DEGREES OF FREEDOM (MECHANICS); FEEDBACK CONTROL; LINEAR CONTROL SYSTEMS; LYAPUNOV METHODS; MATHEMATICAL MODELS; MODAL ANALYSIS; PROBABILITY; ROBUSTNESS (CONTROL SYSTEMS); SYSTEM STABILITY;

AERODYNAMIC UNCERTAINTIES; SKID-TO-TURN MISSILES;

MISSILES;

EID: 0033736470     PISSN: 00189251     EISSN: None     Source Type: None    
DOI: 10.1109/7.845225     Document Type: Article

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