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Volumn , Issue , 1993, Pages 710-719
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Design of a flight control system for a highly maneuverable aircraft using µ synthesis
a a a |
Author keywords
[No Author keywords available]
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Indexed keywords
AERODYNAMICS;
AIRCRAFT CONTROL;
ANGLE OF ATTACK;
ANGLE OF ATTACK INDICATORS;
CONTROL SYSTEM SYNTHESIS;
DESIGN;
FLIGHT CONTROL SYSTEMS;
QUALITY CONTROL;
UNCERTAINTY ANALYSIS;
VEHICLE PERFORMANCE;
CONTROL ACTUATORS;
CONTROLLER DESIGNS;
HIGH PERFORMANCE AIRCRAFTS;
LONGITUDINAL CONTROLLERS;
MODEL UNCERTAINTIES;
NONLINEAR SIMULATIONS;
STRUCTURED SINGULAR VALUES;
SYNTHESIS PROCEDURE;
CONTROLLERS;
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EID: 84959136443
PISSN: None
EISSN: None
Source Type: Conference Proceeding
DOI: None Document Type: Conference Paper |
Times cited : (7)
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References (11)
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