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Volumn , Issue , 1996, Pages 1-6
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Optimal setpoint controller for a generic X-29A aircraft with forebody vortex nozzles
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Author keywords
[No Author keywords available]
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Indexed keywords
AERODYNAMICS;
AIRCRAFT;
BANG BANG CONTROL SYSTEMS;
CLOSED LOOP CONTROL SYSTEMS;
FEEDBACK CONTROL;
FLOW CONTROL;
MATHEMATICAL MODELS;
NOZZLES;
VELOCITY;
VORTEX FLOW;
AERODYNAMIC CONTROL EFFECTORS;
ALTITUDE;
ANGLE OF ATTACK;
DYNAMIC PRESSURE;
FOREBODY VORTEX NOZZLES;
LINEAR TIME INVARIANT GENERIC MODEL;
OPTIMAL SETPOINT CONTROLLER;
CONTROL EQUIPMENT;
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EID: 0030364991
PISSN: None
EISSN: None
Source Type: Conference Proceeding
DOI: None Document Type: Conference Paper |
Times cited : (8)
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References (17)
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