Iterative Sliding Mode and Increment Feedback Attitude Control for On-Orbit Capturing Process of Spacecraft

Iterative Sliding Mode and Increment Feedback Attitude Control for On-Orbit Capturing Process of Spacecraft

According to the characteristics of spacecraft capturing noncooperative targets in orbit, an increment feedback controller based on nonlinear iterative sliding mode is presented. Firstly, the attitude tracking error equation is established, and then, an increment feedback control law based on bounde...

Full description

Bibliographic Details
Main Authors: ChunWu Yin, YouJun Ding, LiJun Song, ZhaoQiang Li, Xing He
Format: Article
Language:English
Published: Hindawi Limited 2021-01-01
Series:Mathematical Problems in Engineering
Online Access:http://dx.doi.org/10.1155/2021/6622685
id doaj-0a6d00eea1164313808cb502593ea47e
record_format Article
spelling doaj-0a6d00eea1164313808cb502593ea47e2021-02-15T12:53:09ZengHindawi LimitedMathematical Problems in Engineering1024-123X1563-51472021-01-01202110.1155/2021/66226856622685Iterative Sliding Mode and Increment Feedback Attitude Control for On-Orbit Capturing Process of SpacecraftChunWu Yin0YouJun Ding1LiJun Song2ZhaoQiang Li3Xing He4School of Information and Control Engineering, Xi’an University of Architecture and Technology, Xi’an 710055, Shaanxi, ChinaSchool of Information and Control Engineering, Xi’an University of Architecture and Technology, Xi’an 710055, Shaanxi, ChinaSchool of Information and Control Engineering, Xi’an University of Architecture and Technology, Xi’an 710055, Shaanxi, ChinaSchool of Information and Control Engineering, Xi’an University of Architecture and Technology, Xi’an 710055, Shaanxi, ChinaSchool of Information and Control Engineering, Xi’an University of Architecture and Technology, Xi’an 710055, Shaanxi, ChinaAccording to the characteristics of spacecraft capturing noncooperative targets in orbit, an increment feedback controller based on nonlinear iterative sliding mode is presented. Firstly, the attitude tracking error equation is established, and then, an increment feedback control law based on bounded iterative sliding modes is proposed, which does not need to estimate the uncertain moment of inertia and external disturbances. For comparing, an adaptive sliding mode controller has been designed in the paper. Some numerical simulations have been given in the presence of spacecraft on-orbit capturing noncooperative target, and the simulation results show that the increment feedback controller has strong robustness to the unknown parametric variations and external disturbances and has a smaller control input torque in control process.http://dx.doi.org/10.1155/2021/6622685
collection DOAJ
language English
format Article
sources DOAJ
author ChunWu Yin
YouJun Ding
LiJun Song
ZhaoQiang Li
Xing He
spellingShingle ChunWu Yin
YouJun Ding
LiJun Song
ZhaoQiang Li
Xing He
Iterative Sliding Mode and Increment Feedback Attitude Control for On-Orbit Capturing Process of Spacecraft
Mathematical Problems in Engineering
author_facet ChunWu Yin
YouJun Ding
LiJun Song
ZhaoQiang Li
Xing He
author_sort ChunWu Yin
title Iterative Sliding Mode and Increment Feedback Attitude Control for On-Orbit Capturing Process of Spacecraft
title_short Iterative Sliding Mode and Increment Feedback Attitude Control for On-Orbit Capturing Process of Spacecraft
title_full Iterative Sliding Mode and Increment Feedback Attitude Control for On-Orbit Capturing Process of Spacecraft
title_fullStr Iterative Sliding Mode and Increment Feedback Attitude Control for On-Orbit Capturing Process of Spacecraft
title_full_unstemmed Iterative Sliding Mode and Increment Feedback Attitude Control for On-Orbit Capturing Process of Spacecraft
title_sort iterative sliding mode and increment feedback attitude control for on-orbit capturing process of spacecraft
publisher Hindawi Limited
series Mathematical Problems in Engineering
issn 1024-123X
1563-5147
publishDate 2021-01-01
description According to the characteristics of spacecraft capturing noncooperative targets in orbit, an increment feedback controller based on nonlinear iterative sliding mode is presented. Firstly, the attitude tracking error equation is established, and then, an increment feedback control law based on bounded iterative sliding modes is proposed, which does not need to estimate the uncertain moment of inertia and external disturbances. For comparing, an adaptive sliding mode controller has been designed in the paper. Some numerical simulations have been given in the presence of spacecraft on-orbit capturing noncooperative target, and the simulation results show that the increment feedback controller has strong robustness to the unknown parametric variations and external disturbances and has a smaller control input torque in control process.
url http://dx.doi.org/10.1155/2021/6622685
work_keys_str_mv AT chunwuyin iterativeslidingmodeandincrementfeedbackattitudecontrolforonorbitcapturingprocessofspacecraft
AT youjunding iterativeslidingmodeandincrementfeedbackattitudecontrolforonorbitcapturingprocessofspacecraft
AT lijunsong iterativeslidingmodeandincrementfeedbackattitudecontrolforonorbitcapturingprocessofspacecraft
AT zhaoqiangli iterativeslidingmodeandincrementfeedbackattitudecontrolforonorbitcapturingprocessofspacecraft
AT xinghe iterativeslidingmodeandincrementfeedbackattitudecontrolforonorbitcapturingprocessofspacecraft
_version_ 1714866446992932864

Similar Items