Multifarious Chaotic Attractors and Its Control in Rigid Body Attitude Dynamical System
The Euler dynamical equation which describes the attitude motion of a rigid body will exhibit very complex dynamic behaviors under the action of different external torques. Many special types of new chaotic attractors are presented, including hidden attractors, double-body-double-core chaotic attrac...
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2020-01-01
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Series: | Mathematical Problems in Engineering |
Online Access: | http://dx.doi.org/10.1155/2020/5958768 |
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doaj-5f1f03666c0f43fe8909e5736e1ed2002020-11-30T09:11:28ZengHindawi LimitedMathematical Problems in Engineering1024-123X1563-51472020-01-01202010.1155/2020/59587685958768Multifarious Chaotic Attractors and Its Control in Rigid Body Attitude Dynamical SystemYang Wang0Zhen Wang1Dezhi Kong2Lingyun Kong3Yukun Qiao4School of Science, Xijing University, Xi’an 710123, ChinaSchool of Science, Xijing University, Xi’an 710123, ChinaSchool of Mechanical Engineering, Northwestern Polytechnical University, Xi’an 710072, ChinaSchool of Science, Xijing University, Xi’an 710123, ChinaSchool of Science, Xijing University, Xi’an 710123, ChinaThe Euler dynamical equation which describes the attitude motion of a rigid body will exhibit very complex dynamic behaviors under the action of different external torques. Many special types of new chaotic attractors are presented, including hidden attractors, double-body-double-core chaotic attractors, and single-body-three-core-tree-wing chaotic attractors. The position of equilibrium points in several typical cases of the Euler dynamic equation is solved, and the stability of linearized equation at each equilibrium point and its influence on the formation of the chaotic attractor are analyzed. An improved nonlinear relay control law based on Euler angle feedback is developed to stabilize a new chaotic spacecraft attitude motion to an appointed equilibrium point or a periodic orbit.http://dx.doi.org/10.1155/2020/5958768 |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Yang Wang Zhen Wang Dezhi Kong Lingyun Kong Yukun Qiao |
spellingShingle |
Yang Wang Zhen Wang Dezhi Kong Lingyun Kong Yukun Qiao Multifarious Chaotic Attractors and Its Control in Rigid Body Attitude Dynamical System Mathematical Problems in Engineering |
author_facet |
Yang Wang Zhen Wang Dezhi Kong Lingyun Kong Yukun Qiao |
author_sort |
Yang Wang |
title |
Multifarious Chaotic Attractors and Its Control in Rigid Body Attitude Dynamical System |
title_short |
Multifarious Chaotic Attractors and Its Control in Rigid Body Attitude Dynamical System |
title_full |
Multifarious Chaotic Attractors and Its Control in Rigid Body Attitude Dynamical System |
title_fullStr |
Multifarious Chaotic Attractors and Its Control in Rigid Body Attitude Dynamical System |
title_full_unstemmed |
Multifarious Chaotic Attractors and Its Control in Rigid Body Attitude Dynamical System |
title_sort |
multifarious chaotic attractors and its control in rigid body attitude dynamical system |
publisher |
Hindawi Limited |
series |
Mathematical Problems in Engineering |
issn |
1024-123X 1563-5147 |
publishDate |
2020-01-01 |
description |
The Euler dynamical equation which describes the attitude motion of a rigid body will exhibit very complex dynamic behaviors under the action of different external torques. Many special types of new chaotic attractors are presented, including hidden attractors, double-body-double-core chaotic attractors, and single-body-three-core-tree-wing chaotic attractors. The position of equilibrium points in several typical cases of the Euler dynamic equation is solved, and the stability of linearized equation at each equilibrium point and its influence on the formation of the chaotic attractor are analyzed. An improved nonlinear relay control law based on Euler angle feedback is developed to stabilize a new chaotic spacecraft attitude motion to an appointed equilibrium point or a periodic orbit. |
url |
http://dx.doi.org/10.1155/2020/5958768 |
work_keys_str_mv |
AT yangwang multifariouschaoticattractorsanditscontrolinrigidbodyattitudedynamicalsystem AT zhenwang multifariouschaoticattractorsanditscontrolinrigidbodyattitudedynamicalsystem AT dezhikong multifariouschaoticattractorsanditscontrolinrigidbodyattitudedynamicalsystem AT lingyunkong multifariouschaoticattractorsanditscontrolinrigidbodyattitudedynamicalsystem AT yukunqiao multifariouschaoticattractorsanditscontrolinrigidbodyattitudedynamicalsystem |
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1715027798512369664 |