Dual Quaternion Based Close Proximity Operation for In-Orbit Assembly via Model Predictive Control

This paper studies the problem of guidance and control for autonomous in-orbit assembly. A six-degree-of-freedom (6-DOF) motion control for in-orbit assembly close proximity operation between a service satellite and a target satellite is addressed in detail. The dynamics based on dual quaternion are...

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Autores principales:	Chuqi Sun, Yan Xiao, Zhaowei Sun, Dong Ye
Formato:	article
Lenguaje:	EN
Publicado:	Hindawi Limited 2021
Materias:	Motor vehicles. Aeronautics. Astronautics TL1-4050
Acceso en línea:	https://doaj.org/article/84e0e9dfaf4144c091f18b54f468ecf4
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id	oai:doaj.org-article:84e0e9dfaf4144c091f18b54f468ecf4
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spelling	oai:doaj.org-article:84e0e9dfaf4144c091f18b54f468ecf42021-11-22T01:10:13ZDual Quaternion Based Close Proximity Operation for In-Orbit Assembly via Model Predictive Control1687-597410.1155/2021/1305095https://doaj.org/article/84e0e9dfaf4144c091f18b54f468ecf42021-01-01T00:00:00Zhttp://dx.doi.org/10.1155/2021/1305095https://doaj.org/toc/1687-5974This paper studies the problem of guidance and control for autonomous in-orbit assembly. A six-degree-of-freedom (6-DOF) motion control for in-orbit assembly close proximity operation between a service satellite and a target satellite is addressed in detail. The dynamics based on dual quaternion are introduced to dispose the coupling effect between translation and rotation in a succinct frame, in which relevant perturbation and disturbance are involved. With the consideration of economical principle for fuel consume, a generic control system based on model predictive control (MPC) is then designed to generate a suboptimal control sequence for rendezvous trajectory considering actuator output saturation. The stability and robustness issues of the MPC-based control system are analyzed and proved. Numerical simulations are presented to demonstrate the effectiveness and robustness of the proposed control scheme, while additional comparisons for diverse horizons of the MPC are further conducted.Chuqi SunYan XiaoZhaowei SunDong YeHindawi LimitedarticleMotor vehicles. Aeronautics. AstronauticsTL1-4050ENInternational Journal of Aerospace Engineering, Vol 2021 (2021)
institution	DOAJ
collection	DOAJ
language	EN
topic	Motor vehicles. Aeronautics. Astronautics TL1-4050
spellingShingle	Motor vehicles. Aeronautics. Astronautics TL1-4050 Chuqi Sun Yan Xiao Zhaowei Sun Dong Ye Dual Quaternion Based Close Proximity Operation for In-Orbit Assembly via Model Predictive Control
description	This paper studies the problem of guidance and control for autonomous in-orbit assembly. A six-degree-of-freedom (6-DOF) motion control for in-orbit assembly close proximity operation between a service satellite and a target satellite is addressed in detail. The dynamics based on dual quaternion are introduced to dispose the coupling effect between translation and rotation in a succinct frame, in which relevant perturbation and disturbance are involved. With the consideration of economical principle for fuel consume, a generic control system based on model predictive control (MPC) is then designed to generate a suboptimal control sequence for rendezvous trajectory considering actuator output saturation. The stability and robustness issues of the MPC-based control system are analyzed and proved. Numerical simulations are presented to demonstrate the effectiveness and robustness of the proposed control scheme, while additional comparisons for diverse horizons of the MPC are further conducted.
format	article
author	Chuqi Sun Yan Xiao Zhaowei Sun Dong Ye
author_facet	Chuqi Sun Yan Xiao Zhaowei Sun Dong Ye
author_sort	Chuqi Sun
title	Dual Quaternion Based Close Proximity Operation for In-Orbit Assembly via Model Predictive Control
title_short	Dual Quaternion Based Close Proximity Operation for In-Orbit Assembly via Model Predictive Control
title_full	Dual Quaternion Based Close Proximity Operation for In-Orbit Assembly via Model Predictive Control
title_fullStr	Dual Quaternion Based Close Proximity Operation for In-Orbit Assembly via Model Predictive Control
title_full_unstemmed	Dual Quaternion Based Close Proximity Operation for In-Orbit Assembly via Model Predictive Control
title_sort	dual quaternion based close proximity operation for in-orbit assembly via model predictive control
publisher	Hindawi Limited
publishDate	2021
url	https://doaj.org/article/84e0e9dfaf4144c091f18b54f468ecf4
work_keys_str_mv	AT chuqisun dualquaternionbasedcloseproximityoperationforinorbitassemblyviamodelpredictivecontrol AT yanxiao dualquaternionbasedcloseproximityoperationforinorbitassemblyviamodelpredictivecontrol AT zhaoweisun dualquaternionbasedcloseproximityoperationforinorbitassemblyviamodelpredictivecontrol AT dongye dualquaternionbasedcloseproximityoperationforinorbitassemblyviamodelpredictivecontrol
_version_	1718418350017609728

Dual Quaternion Based Close Proximity Operation for In-Orbit Assembly via Model Predictive Control

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