2012
DOI: 10.2322/tjsass.55.265
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Adjustable Adaptive Fuzzy Attitude Control using Nonlinear SISO Structure of Satellite Dynamics

Abstract: This paper presents a method for three-dimensional attitude stabilization of a satellite. The pitch loop of the satellite is controlled by a momentum wheel; whereas the roll/yaw loops are stabilized using two magnetic torques along their respective axes. In order to design an efficient controller, the stability conditions are considered based on a nonlinear model of system. An adjustable adaptive fuzzy system is proposed as the method to design the controller. The span of membership functions are tuned using e… Show more

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Cited by 2 publications
(2 citation statements)
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References 28 publications
(25 reference statements)
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“…Stabilizing a space robot with un-modeled uncertainties and external perturbations is a tedious task. In the literature, there are different methods such as the adaptive control, 20 H_∞ control, fuzzy control, 21 optimal control, and feedback linearization 22 to list a few. Although these non-linear robust control methods result in high performance and robustness, solving the associated Hamilton-Jacobi equation is often extremely complicated, and requires huge computational power; therefore, it makes the resulting controller hard to implement on the AOCS systems.…”
Section: Pid Controllermentioning
confidence: 99%
“…Stabilizing a space robot with un-modeled uncertainties and external perturbations is a tedious task. In the literature, there are different methods such as the adaptive control, 20 H_∞ control, fuzzy control, 21 optimal control, and feedback linearization 22 to list a few. Although these non-linear robust control methods result in high performance and robustness, solving the associated Hamilton-Jacobi equation is often extremely complicated, and requires huge computational power; therefore, it makes the resulting controller hard to implement on the AOCS systems.…”
Section: Pid Controllermentioning
confidence: 99%
“…Effectiveness of their proposed fault diagnosis methodology was demonstrated by utilizing synthetic formation flying data of five satellites that were configured in the leader-follower architecture. Moradi et al [21] presented a method for three-dimensional attitude stabilization of a satellite. The pitch loop of the satellite was controlled by a momentum wheel; whereas the roll/yaw loops were stabilized by using two magnetic torques along their respective axes.…”
Section: Fuzzy Set Theory In Astronomy and Astrophysicsmentioning
confidence: 99%