MODIFICATIONS OF CONTROL ACTUATION SYSTEMS OF ATGM
Abstract eng: 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.
Contributors:
Publisher:
Brno University of Technology, Institute of Solid Mechanics, Mechatronics and Biomechanics, Brno
Conference Title:
Conference Title:
Engineering Mechanics 2017
Conference Venue:
Svratka, CZ
Conference Dates:
2017-05-15 / 2017-05-18
Rights:
Text je chráněný podle autorského zákona č. 121/2000 Sb.
Record appears in:
Record created 2017-05-22, last modified 2017-05-22
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