Sliding Mode Control for a Gyroscope System

Abstract

This paper presents a mathematical model of a gyroscope system with a sliding mode controller. A comparative analysis based on various control algorithms implemented in a controlled gyroscope system installed on a mobile platform (such as an UAV or a homing rocket missile) proved that sliding mode control can be highly effective, especially when external input interferences exist with the kinematic reactions of the mobile platform. A gyroscope system with a sliding mode controller can be used in the optical target seeker systems of precision weapons. The simulation results are provided in a graphical format.

Authors and Affiliations

Izabela KRZYSZTOFIK, Zbigniew KORUBA

Keywords

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  • EP ID EP246208
  • DOI 10.5604/01.3001.0010.7317
  • Views 88
  • Downloads 0

How To Cite

Izabela KRZYSZTOFIK, Zbigniew KORUBA (2017). Sliding Mode Control for a Gyroscope System. Problemy Mechatroniki. Uzbrojenie, lotnictwo, inżynieria bezpieczeństwa, 8(4), 47-60. https://europub.co.uk./articles/-A-246208