Impulsive Control of Attitude Satellite With Quaternion Parameters
الموضوعات : مجله بین المللی ریاضیات صنعتی
M. R. Niknam
1
(Department of Mathematics, Khalkhal Branch, Islamic Azad University, Khalkhal, Iran.)
N. Abdi Sobouhi
2
(Department of Education, Farhangian University, Tabriz, Iran.)
الکلمات المفتاحية: Satellite attitude, Lyapunov exponent, Impulsive control, Quaternion, Chaotic system,
ملخص المقالة :
This article uses impulsive control along with quaternion parameters instead of Euler angles in kinematics equations of satellite. ‎The quaternion parameters are applied to overcome singularity problem in the numerical solution. ‎It is assumed that the satellite is subjected to deterministic external perturbations. ‎At first, ‎the chaotic behavior of system is investigated when there is no control on the system. ‎Then, ‎impulsive control is used to stabilize the satellite attitude around the equilibrium point of origin. ‎Finally, ‎simulation results are given to visualize the effectiveness and feasibility of the proposed ‎method.
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