Design of an Adaptive-Neural Network Attitude Controller of a Satellite using Reaction Wheels
سال انتشار: 1394
نوع سند: مقاله ژورنالی
زبان: انگلیسی
مشاهده: 389
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شناسه ملی سند علمی:
JR_JACM-1-2_003
تاریخ نمایه سازی: 9 خرداد 1396
چکیده مقاله:
In this paper, an adaptive attitude control algorithm is developed based on neural network for a satellite using four reaction wheels in a tetrahedron configuration. Then, an attitude control based on feedback linearization control has been designed and uncertainties in the moment of inertia matrix and disturbances torque have been considered. In order to eliminate the effect of these uncertainties, a multilayer neural network with back-propagation law is designed. In this structure, the parameters of the moment of inertiamatrix and external disturbances are estimated and used in feedback linearization control law. Finally, the performance of the designed attitude controller is investigated by several simulations
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نویسندگان
Abbas Ajorkar
Department of Mechanical Engineering, Amirkabir University of Technology Hafez Street, Tehran, 15875-4413, Iran
Alireza Fazlyab
Department of Mechanical Engineering, Amirkabir University of Technology Hafez Street, Tehran, 15875-4413, Iran
Farhad Fani Saberi
Space Science and Technology Institute, Amirkabir University of Technology Hafez Street, Tehran, 15875-4413, Iran
Mansour Kabganian
Department of Mechanical Engineering, Amirkabir University of Technology Hafez Street, Tehran, 15875-4413, Iran