Three dimensional interpolation method for missile aerodynamics
Three dimensional interpolation method for missile aerodynamics
The computer simulation of missile flight dynamics requires missile aerodynamic stability coefficients as continuous functions of flight parameters. Presently, the accurate information on missile aerodynamic characteristics is mainly derived from measurements on a missile scale model in the wind tunnel. The use of wind tunnel data in six-degree-of-freedom simulation programs involves interpolation of the test data. A compact, fast and accurate three dimensional (Mach, roll attitude and angle of attack) interpolation method is presented.
Document information
Three dimensional interpolation method for missile aerodynamics
Dreidimensionale Interpolationsmethode fuer die Aerodynamik von Raketen
AIAA-Papers ; Jan ; 1-11
1988
11 Seiten, 19 Bilder, 10 Quellen
Conference paper
English
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