Providing carrier rocket motion controllability on the basis of design smoothed wind profile application

Abstract

An algorithm of smoothed wind profile calculating on the basis of the data of atmospheric sounding before the carrier rocket launch has been developed. A method of using design smoothed wind profile in the carrier rocket first stage ascent program for the purpose of providing the controllability under intensive wind perturbations.

About the authors

Ye. A. Yendutkina

State Research and Production Space Rocket Center “TsSKB – Progress”, Samara

Author for correspondence.
Email: endutkina.ea@mail.ru

Head of Group

Russian Federation

B. A. Titov

Samara State Aerospace University

Email: Titov@ssau.ru

Doctor of Technical Sciences, Professor

Head of the Department of Logistics and Management in Transport

Russian Federation

References

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