Attitude control of missile via fliess expansion

IEEE Transactions on Control Systems Technology

Volumn 16, Issue 5, 2008, Pages 959-970

  Yao, Yu ^a   Yang, Baoqing ^a   He, Fenghua ^a   Qiao, Yupeng ^b   Cheng, Daizhan ^b  

^a HARBIN INSTITUTE OF TECHNOLOGY   (China)

^b INSTITUTE OF SYSTEMS SCIENCE   (China)

Author keywords

Attitude control; Fliess functional expansion; Model predictive tracking control; Nonlinear system

Indexed keywords

ATTITUDE CONTROL; CONTROL SYSTEMS; MILITARY EQUIPMENT; MISSILES; NAVIGATION; NONLINEAR SYSTEMS; ORDNANCE; PARAMETER ESTIMATION; PREDICTIVE CONTROL SYSTEMS; SPATIAL VARIABLES CONTROL; UNCERTAINTY ANALYSIS;

FLIESS FUNCTIONAL EXPANSION; FUNCTIONAL EXPANSION; MODEL PREDICTIVE TRACKING CONTROL; MODEL UNCERTAINTIES; NONLINEAR SYSTEM; OPTIMAL CONTROL; SIMULATION RESULTS; SYSTEM'S DYNAMICS; TRACKING PROBLEMS; UNCERTAIN PARAMETERS;

MODEL PREDICTIVE CONTROL;

EID: 49249111833     PISSN: 10636536     EISSN: None     Source Type: Journal    
DOI: 10.1109/TCST.2007.916352     Document Type: Article

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