Intelligent adaptive control of a Tailless Advanced Fighter Aircraft under wing damage

Journal of Guidance, Control, and Dynamics

Volumn 23, Issue 5, 2000, Pages 876-884

  Bošković, Jovan D ^a   Mehra, Raman K ^a  

^a SCIENTIFIC SYSTEMS COMPANY INC   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; COMPUTER SIMULATION; CONTROL SYSTEM ANALYSIS; CONTROL SYSTEM SYNTHESIS; CONVERGENCE OF NUMERICAL METHODS; ERROR ANALYSIS; FIGHTER AIRCRAFT; FLIGHT DYNAMICS; INTELLIGENT CONTROL; MATHEMATICAL MODELS; OBSERVABILITY; SPURIOUS SIGNAL NOISE;

INTELLIGENT ADAPTIVE RECONFIGURABLE CONTROL METHOD;

ADAPTIVE CONTROL SYSTEMS;

EID: 0343441595     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4617     Document Type: Article

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