Engineering Mechanics

Proceedings Vol. 23 (2017)

ENGINEERING MECHANICS 2017

Copyright © 2017 Brno University of Technology, Faculty of Mechanical Engineering, Institute of Solid Mechanics, Mechatronics and Biomechanics, Brno

 

Nocoń Ł., Koruba Z.
pages 714 - 717, full text

The paper presents the modifications of missile control actuation systems. The control actuation system was modified by adding a swiveling nozzle of the rocket engine. In that way, a hybrid control system consisting of aerodynamic rudders and gasodynamic rudders (i.e. change of the direction of the rocket engine thrust). The control effectiveness with the use of aerodynamic rudders alone was compared with ATGM control effectiveness with the use of the hybrid control actuation system. The results of the research are shown in a graphical form.

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