Determination of missile angular position in relation to wind speed changing as per power law

Аuthors

Komissarenko A. I.

Instrument Design Bureau named after academician A.G. Shipunov, 59, Shcheglovskaya Zaseka str., Tula, 300001, Russia

e-mail: kbkedr@tula.net

Abstract

The article relates to determination of the missile angular position under the action of wind velocity which changes according to the power law of altitude function. The missile moves vertically. The analytic dependences of the attack angle, the velocity vector angle of the altitude function and the wind velocity degree which features atmosphere stratification were obtained.

Keywords:

drag, missile trajectory identification