1.2.2019 Optimization of the trajectory of the antiaircraft guided missile

Optimization of the trajectory of the antiaircraft guided missile Authors: Izhko V. 2019, (2); 3-10 DOI: https://doi.org/10.33136/stma2019.02.003 Language: Russian [...]

Read more 1.2.2019 Optimization of the trajectory of the antiaircraft guided missile

12.2.2018 Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs

Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs Authors: Aksyonenko A. The aim of [...]

Read more 12.2.2018 Methodological Support for Initial Phase Optimization of Projecting Design, Trajectory Parameters and Rocket Object Motion Control Programs

2.1.2020 Analysis of development trends of design parameters and basic characteristics of missiles for the advanced multiple launch rocket systems

The formalization of the complex task to optimize design parameters, trajectory parameters and motion control programs for the guided missiles capable of flying along the [...]

Read more 2.1.2020 Analysis of development trends of design parameters and basic characteristics of missiles for the advanced multiple launch rocket systems

7.1.2020 Studying the motion of a launch vehicle and observed space debris objects during launch preparation

It is shown that as the launch moment becomes closer, the cataloged space situation is ascertained, which leads to the constant change of the quantity of hazardous space debris [...]

Read more 7.1.2020 Studying the motion of a launch vehicle and observed space debris objects during launch preparation

17.2.2018 Peculiarities of Dynamics of Recoverable Part of Stage of Aircraft-Type Configuration with Turbojet Engine

This descend trajectory was considered as standard and was used to evaluate the efficiency of the wing and turbojet with relatively small propulsion. The possibility to [...]

Read more 17.2.2018 Peculiarities of Dynamics of Recoverable Part of Stage of Aircraft-Type Configuration with Turbojet Engine

13.2.2018 On an Approach to Constructing the Extremes in the Tasks of Optimal Solutions Search

The use of the latter will allow obtaining new solutions of various problems of technical mechanics, such as the task of determining optimal trajectory parameters of launch [...]

Read more 13.2.2018 On an Approach to Constructing the Extremes in the Tasks of Optimal Solutions Search

11.2.2019 Winding the tubes of rectangular section using dowels

For this purpose, we determine the angles of coil winding, corresponding angles of mandrel turn in determined coordinates X, the coordinates of band escape point, angle of [...]

Read more 11.2.2019 Winding the tubes of rectangular section using dowels