Abstract
In this study, the chaos controllers are improved for the control of satellite attitude motion of the sliding mode control and passive control methods. Sliding mode control has three controller inputs, whereas passive control has only one controller input. The control structure of satellite attitude motion chaotic system was theoretically calculated, and then applied to numerical examples. Both the sliding mode and passive control methods reached to an equilibrium point, but the results of the simulations sliding mode control were better performed than the passive control method. The results show that the method of sliding mode compares very favorable with the passive control method.
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