Design of missile guidance law via variable structure control

Journal of Guidance, Control, and Dynamics

Volumn 24, Issue 4, 2001, Pages 659-664

  Moon, Jongki ^a,b   Kim, Kiseok ^a,b   Kim, Youdan ^a,c  

^a Seoul National University   (South Korea)

^b Department of Aerospace Engineering ^*  (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION; CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; CONTROL SYSTEM SYNTHESIS; DIFFERENTIAL EQUATIONS; KINEMATICS; MANEUVERABILITY; ROBUSTNESS (CONTROL SYSTEMS); SLIDING MODE CONTROL;

MISSILE GUIDANCE LAW; NONLINEAR PLANAR ENGAGEMENT KINEMATICS; VARIABLE STRUCTURE CONTROL;

ELECTRONIC GUIDANCE SYSTEMS;

EID: 0035393352     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4792     Document Type: Article

References (21)

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