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Volumn , Issue , 2002, Pages
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Design, development and flight testing of control laws for the Indian light combat aircraft
b
C V Raman Nagar
(India)
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Author keywords
[No Author keywords available]
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Indexed keywords
AERODYNAMIC STABILITY;
AIRCRAFT CONTROL;
CONTROL THEORY;
DELTA WING AIRCRAFT;
FLIGHT CONTROL SYSTEMS;
FLIGHT ENVELOPES;
FLIGHT SIMULATORS;
LIFE CYCLE;
QUALITY CONTROL;
SUPERSONIC AIRCRAFT;
VEHICLE PERFORMANCE;
WINGS;
AIRCRAFT EXTERNAL STORES;
AIRCRAFT PERFORMANCE;
DEVELOPMENT AND TESTING;
ENTIRE FLIGHT ENVELOPE;
FLIGHT CONTROL LAW;
LIGHT COMBAT AIRCRAFTS;
LONGITUDINAL AXIS;
STABILITY AND CONTROL;
FIGHTER AIRCRAFT;
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EID: 85048706235
PISSN: None
EISSN: None
Source Type: Conference Proceeding
DOI: 10.2514/6.2002-4649 Document Type: Conference Paper |
Times cited : (17)
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References (6)
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