Дослідження режимів та ідентифікація параметрів моделі системи наведення та стабілізації бойових машин

Abstract

The variant of the computer model of the electric drive of the multiple rocket launcher guides is proposed in this article. The identification of the mechanical parts of drive based on experimental data's including their features such as Coulomb and viscous friction and springiness of the guides mechanism was used for model description.