A comparing design of satellite attitude control system based on reaction wheel |
| |
Authors: | CHENG Hao GE Sheng-min SHEN Yi |
| |
Affiliation: | Dept.of Control Science and Engineering,School of Astronautics,Harbin Institute of Technology,Harbin 150001,China |
| |
Abstract: | The disturbance caused by the reaction wheel with a current controller greatly influences the accuracy and stability of the satellite attitude control system.To solve this problem,the idea of speed feedback compensation control reaction wheel is put forward.This paper introduces the comparison on design and performance of two satellite attitude control systems,which are separately based on the current control reaction wheel and the speed feedback compensation control reaction wheel.Analysis shows that the speed feedback compensation control flywheel system may effectively suppress the torque fluctuation.Simulation results indicate that the satellite attitude control system with the speed feedback compensation control flywheel has improved performance. |
| |
Keywords: | compensation control reaction wheel attitude control |
本文献已被 CNKI 维普 万方数据 等数据库收录! |