Robust stochastic controller for a missile guidance system

Proceedings of the IEEE International Conference on Electronics, Circuits, and Systems

Volumn 2, Issue , 2000, Pages 793-796

  Rizk, M R M ^a   Rahim, M Abdel ^a  

^a Alexandria University The Faculty Of Engineering   (Egypt)

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATE EQUATION; CENTER OF GRAVITY; CONTROL SCHEMES; DEGREE OF STABILITY; DISCRETE FORM; DISCRETE-TIME; HORIZONTAL PLANES; KINEMATIC EQUATIONS; MISSILE GUIDANCE SYSTEMS; NON-LINEAR STOCHASTIC SYSTEMS; NUMERICAL EXAMPLE; PROCESS EQUATION; REFERENCE STATE; ROTARY MOTIONS; STABILIZING PROPERTIES; STATE FEEDBACK CONTROLLER; SYSTEM STATE; TARGET IMPACT; VERTICAL PLANE;

CONTROLLERS; DISCRETE TIME CONTROL SYSTEMS; ELECTRONIC GUIDANCE SYSTEMS; EQUATIONS OF MOTION; FEEDBACK; MISSILES; NONLINEAR EQUATIONS; STATE FEEDBACK; STOCHASTIC CONTROL SYSTEMS; STOCHASTIC SYSTEMS; WHITE NOISE;

PROCESS CONTROL;

EID: 77956038210     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/ICECS.2000.912996     Document Type: Conference Paper

References (10)

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