Autopilot design for bank-to-turn missiles using receding horizon predictive control scheme

Journal of Guidance, Control, and Dynamics

Volumn 20, Issue 6, 1997, Pages 1248-1254

  Kim, Myung Joon ^a,c   Kwon, Wook Hyun ^a,c   Kim, Yong Ho ^a,c   Song, Chanho ^b,d  

^a Seoul National University   (South Korea)

^b Agency for Defence Development   (South Korea)

^c Departrnent of Aerospace Engineering   (South Korea)

^d Guid and Contr Technology Division

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; APPROXIMATION THEORY; COMMAND AND CONTROL SYSTEMS; COMPUTER SIMULATION; DEGREES OF FREEDOM (MECHANICS); ELECTRONIC GUIDANCE SYSTEMS; MANEUVERABILITY; MISSILES; MOTION CONTROL;

BANK TO TURN MISSILES; RECEDING HORIZON PREDICTIVE CONTROL;

PREDICTIVE CONTROL SYSTEMS;

EID: 0031271762     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4184     Document Type: Article

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