DETERMINATION OF THE OPTIMAL CONTROL LAW FOR SOLAR SECTIONS TRANSPORTATION TO THE ISS

A.L. Zhupiev¹, A.A. Sirchenko², S.A. Kelbukova³

¹Senior lecturer of Mining Machines and Engineering Department

²Research scientist of Mining Machines and Engineering Department

³Student, e-mail: kelbukova@gmail.com

^1,2,3State Higher Educational Institution “National Mining University”, Dnepropetrovsk, Ukraine

Abstract. In this work considered the defining of the rocket engine design parameters, including the number and location of the rocket nozzles, and the optimal engine control law for transporting the section.

Keywords: mover, transportation sections, optimization, conceptual model, SolidWorks Motion.