Geodesic
Principles of forming of the wind profiles, used for the flight programme aimed at reduction of loading on the carrier rocket
Vestnik Samarskogo universiteta. Estestvennonaučnaâ seriâ, no. 8 (2009), pp. 118-124

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One of the primal functions of a carrier rocket control system consists in assurance of motion stability under wind impact conditions. Here a technique for forming of wind profiles used for the calculation of ascent programs done according to pre-launch measurements of wind speed is proposed.
Keywords: carrier rocket, control system, motion stability, angle of incidence (slide), atmospheric sounding, wind profile, carrier rocket ascent program. 
@article{VSGU_2009_8_a11,
     author = {V. V. Dmitriev and E. A. Endutkina},
     title = {Principles of forming of the wind profiles, used for the flight programme aimed at reduction of loading on the carrier rocket},
     journal = {Vestnik Samarskogo universiteta. Estestvennonau\v{c}na\^a seri\^a},
     pages = {118--124},
     publisher = {mathdoc},
     number = {8},
     year = {2009},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/VSGU_2009_8_a11/}
}
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V. V. Dmitriev; E. A. Endutkina. Principles of forming of the wind profiles, used for the flight programme aimed at reduction of loading on the carrier rocket. Vestnik Samarskogo universiteta. Estestvennonaučnaâ seriâ, no. 8 (2009), pp. 118-124. http://geodesic.mathdoc.fr/item/VSGU_2009_8_a11/