Framework for establishing the limits of tabular aerodynamic models for flight dynamics analysis

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2009, Pages

  Ghoreyshi, M ^a   Badcock, K J ^a   Da Ronch, A ^a   Marques, S ^a   Swift, A ^a   Ames, N ^a  

^a UNIVERSITY OF LIVERPOOL   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC MODELS; ANGLES OF ATTACK; DYNAMICS ANALYSIS; DYNAMICS MODELS; MOTION RATE; OPTIMISATIONS; STATIC AND DYNAMIC; TEST CASE; TIME-ACCURATE CFD; TIME-OPTIMAL; UNSTEADY EFFECTS; VORTICAL FLOWS; WIND-TUNNEL DATA;

AIRCRAFT CONTROL; COMPUTATIONAL FLUID DYNAMICS; DYNAMICS; FLIGHT DYNAMICS; GAS DYNAMICS; NAVIGATION; OPTIMIZATION; WIND TUNNELS;

CONTROL SURFACES;

EID: 78049271362     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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