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Optimal attitude control of a satellite in real orbit using multiple fractional-order controllers


Affiliations
1 Mechanical engineering, materials, and structures laboratory, Faculty of Science and Technology, University of Tissemsilt, Algeria
2 Institute of Aeronautics and Space Studies, Saad Dahlab University, Blida,, Algeria
3 Faculty of Science and Technology, University of Djelfa, Algeria
 

The purpose of this work is to design three optimal fractional-order PIλ D µ controllers for regulating the attitude of a three-axis satellite. The parameter gains of the controllers are tuned with the innovative Harris Hawks Optimizer (HHO). The state-space dynamic model of the satellite system is obtained by linearizing the nonlinear model around the Local Horizontal Local Vertical (LHLV) orbital frame. This allows for the model to be solved in state space. A study in which conventional PID controllers were used as a point of comparison was carried out so that it could be shown how valuable the fractional order is in the design that was proposed.

Keywords

Satellite system, Attitude control, PID Controller, Fractional-order, Harris Hawks Optimizer.
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  • Optimal attitude control of a satellite in real orbit using multiple fractional-order controllers

Abstract Views: 97  |  PDF Views: 66

Authors

Bachir Nail
Mechanical engineering, materials, and structures laboratory, Faculty of Science and Technology, University of Tissemsilt, Algeria
Belkacem Bekhiti
Institute of Aeronautics and Space Studies, Saad Dahlab University, Blida,, Algeria
Mahedi Abdelghani Atoussi
Faculty of Science and Technology, University of Djelfa, Algeria

Abstract


The purpose of this work is to design three optimal fractional-order PIλ D µ controllers for regulating the attitude of a three-axis satellite. The parameter gains of the controllers are tuned with the innovative Harris Hawks Optimizer (HHO). The state-space dynamic model of the satellite system is obtained by linearizing the nonlinear model around the Local Horizontal Local Vertical (LHLV) orbital frame. This allows for the model to be solved in state space. A study in which conventional PID controllers were used as a point of comparison was carried out so that it could be shown how valuable the fractional order is in the design that was proposed.

Keywords


Satellite system, Attitude control, PID Controller, Fractional-order, Harris Hawks Optimizer.

References