1. KUANYSH ALIPBAYEV - Almaty University of Power Engineering and Telecommunications Named After Gumarbek
Daukeyev, Almaty, Kazakhstan.
2. MEREY IBRAIM - Almaty University of Power Engineering and Telecommunications Named After Gumarbek
Daukeyev, Almaty, Kazakhstan.
3. KENZHEBEK MYRZABEKOV - Almaty University of Power Engineering and Telecommunications Named After Gumarbek
Daukeyev, Almaty, Kazakhstan.
4. SERIKBAY KOSBOLOV - Almaty University of Power Engineering and Telecommunications Named After Gumarbek
Daukeyev, Almaty, Kazakhstan.
5. DINMUKHAMMAD YESHEN - Almaty University of Power Engineering and Telecommunications Named After Gumarbek
Daukeyev, Almaty, Kazakhstan.
The article presents the problem of developing a mathematical model for controlling the triaxial orientation of a nanosatellite using three flywheels installed along its main central axes of inertia is considered, and a 3D model of the flywheel is also designed. To solve the problem, it is necessary to determine the law of change of the vector of the control moment or the law of control of the movement of the flywheels, which allows you to transfer the nanosatellite from the current angular position to another required angular position. The model can be a useful tool for developing a system for controlling the orientation of satellites of a similar type operating in real time.
Flywheel, nanosatellite, triaxial orientation, machine.