Control design of spinning rockets based on co-evolutionary optimization

Control Engineering Practice

Volumn 9, Issue 2, 2001, Pages 149-157

  Lee, Ho Il ^a   Sun, Byung Chan ^b   Tahk, Min Jea ^a   Lee, Hungu ^a  

^a Korea Advanced Institute of Science and Technology (KAIST)   (South Korea)

^b Korea Aerospace Research Institute (KARI)   (South Korea)

Author keywords

Aerospace; Attitude control; Complex system; Optimization problems; PID controllers

Indexed keywords

COMPUTER SIMULATION; CONSTRAINT THEORY; CONTROL SYSTEM ANALYSIS; CONTROL SYSTEM SYNTHESIS; DEGREES OF FREEDOM (MECHANICS); LAGRANGE MULTIPLIERS; MATHEMATICAL MODELS; NONLINEAR CONTROL SYSTEMS; OPTIMAL CONTROL SYSTEMS; SOUNDING ROCKETS; UNCERTAIN SYSTEMS;

CO-EVOLUTIONARY AUGMENTED LAGRANGIAN METHOD;

THREE TERM CONTROL SYSTEMS;

ROCKET;

EID: 0035071276     PISSN: 09670661     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0967-0661(00)00102-7     Document Type: Article

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