Sliding Mode Control for a Gyroscope System | Zendy

Izabela Krzysztofik | Zendy; Zbigniew Koruba | Zendy

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Sliding Mode Control for a Gyroscope System

Author(s) -

Izabela Krzysztofik,

Zbigniew Koruba

Publication year - 2017

Publication title -

problems of mechatronics armament aviation safety engineering

Language(s) - English

Resource type - Journals

eISSN - 2720-5266

pISSN - 2081-5891

DOI - 10.5604/01.3001.0010.7317

Subject(s) - gyroscope , missile , kinematics , control theory (sociology) , sliding mode control , controller (irrigation) , control engineering , engineering , control system , mode (computer interface) , computer science , control (management) , artificial intelligence , aerospace engineering , physics , agronomy , electrical engineering , classical mechanics , nonlinear system , quantum mechanics , biology , operating system

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.

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