Proceedings Vol. 23 (2017)
ENGINEERING MECHANICS 2017
May 15 – 18, 2017, Svratka, Czech Republic
Copyright © 2017 Brno University of Technology, Faculty of Mechanical Engineering, Institute of Solid Mechanics, Mechatronics and Biomechanics, Brno
ISSN 1805-8248 (printed)
ISSN 1805-8256 (electronic)
list of papers scientific commitee
pages 530 - 533, full text
Precision of anti-aircraft missile homing depends mainly on correct determination of the current angle between the axis of the gyroscope system and the line of sight. The system of automatic gyroscope control should ensure automatic minimization of that angle, and thus, constant directing of the gyroscope system axis towards the line of sight, i.e. tracking the target by the homing head. This paper presents a sliding controller applied to control the gyroscope system. Subsequently, the dynamics of that system during the process of anti-aircraft missile homing onto a moveable target was studied. Some chosen results of the simulation research were presented graphically.
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All papers were reviewed by members of the scientific committee.