Adaptive super-twisting sliding mode altitude trajectory tracking control for reentry vehicle

This paper addresses the altitude trajectory tracking control problem of reentry vehicle subject to bounded uncertainty. A new continuous adaptive super-twisting sliding mode control (ASTSMC) method is developed based on conventional super-twisting sliding mode control (STSMC) and adaptive gain tech...

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Published inISA transactions Vol. 132; pp. 329 - 337
Main Authors Shen, Ganghui, Xia, Yuanqing, Zhang, Jinhui, Cui, Bing
Format Journal Article
LanguageEnglish
Published United States Elsevier Ltd 01.01.2023
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Online AccessGet full text
ISSN0019-0578
1879-2022
1879-2022
DOI10.1016/j.isatra.2022.06.023

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Abstract This paper addresses the altitude trajectory tracking control problem of reentry vehicle subject to bounded uncertainty. A new continuous adaptive super-twisting sliding mode control (ASTSMC) method is developed based on conventional super-twisting sliding mode control (STSMC) and adaptive gain technique, which can improve tracking accuracy and achieve high control performance. Based on adaptive gain technique, the designed ASTSMC method requires no prior information on uncertainty and avoids the overestimation of control gain, then the unexpected chattering phenomenon is alleviated. By employing fast power rate reaching law and modified fast nonsingular terminal sliding mode (FNTSM) surface, the designed controller achieves faster convergence and stronger robustness than conventional STSMC methods. Furthermore, the finite-time stability of closed-loop system is proved through Lyapunov theory. Simulation results are executed to validate the superiority of the proposed controller. •A novel adaptive super-twisting sliding mode control (ASTSMC) law is proposed to address trajectory tracking problem for reentry vehicle under bounded uncertainty.•The proposed ASTSMC law can resolve the gain overestimation, and it requires no prior information on uncertainty.•By employing fast power rate reaching law, the proposed ASTSMC law achieves fast finite-time convergence and exhibits strong robustness.
AbstractList This paper addresses the altitude trajectory tracking control problem of reentry vehicle subject to bounded uncertainty. A new continuous adaptive super-twisting sliding mode control (ASTSMC) method is developed based on conventional super-twisting sliding mode control (STSMC) and adaptive gain technique, which can improve tracking accuracy and achieve high control performance. Based on adaptive gain technique, the designed ASTSMC method requires no prior information on uncertainty and avoids the overestimation of control gain, then the unexpected chattering phenomenon is alleviated. By employing fast power rate reaching law and modified fast nonsingular terminal sliding mode (FNTSM) surface, the designed controller achieves faster convergence and stronger robustness than conventional STSMC methods. Furthermore, the finite-time stability of closed-loop system is proved through Lyapunov theory. Simulation results are executed to validate the superiority of the proposed controller.
This paper addresses the altitude trajectory tracking control problem of reentry vehicle subject to bounded uncertainty. A new continuous adaptive super-twisting sliding mode control (ASTSMC) method is developed based on conventional super-twisting sliding mode control (STSMC) and adaptive gain technique, which can improve tracking accuracy and achieve high control performance. Based on adaptive gain technique, the designed ASTSMC method requires no prior information on uncertainty and avoids the overestimation of control gain, then the unexpected chattering phenomenon is alleviated. By employing fast power rate reaching law and modified fast nonsingular terminal sliding mode (FNTSM) surface, the designed controller achieves faster convergence and stronger robustness than conventional STSMC methods. Furthermore, the finite-time stability of closed-loop system is proved through Lyapunov theory. Simulation results are executed to validate the superiority of the proposed controller. •A novel adaptive super-twisting sliding mode control (ASTSMC) law is proposed to address trajectory tracking problem for reentry vehicle under bounded uncertainty.•The proposed ASTSMC law can resolve the gain overestimation, and it requires no prior information on uncertainty.•By employing fast power rate reaching law, the proposed ASTSMC law achieves fast finite-time convergence and exhibits strong robustness.
This paper addresses the altitude trajectory tracking control problem of reentry vehicle subject to bounded uncertainty. A new continuous adaptive super-twisting sliding mode control (ASTSMC) method is developed based on conventional super-twisting sliding mode control (STSMC) and adaptive gain technique, which can improve tracking accuracy and achieve high control performance. Based on adaptive gain technique, the designed ASTSMC method requires no prior information on uncertainty and avoids the overestimation of control gain, then the unexpected chattering phenomenon is alleviated. By employing fast power rate reaching law and modified fast nonsingular terminal sliding mode (FNTSM) surface, the designed controller achieves faster convergence and stronger robustness than conventional STSMC methods. Furthermore, the finite-time stability of closed-loop system is proved through Lyapunov theory. Simulation results are executed to validate the superiority of the proposed controller.This paper addresses the altitude trajectory tracking control problem of reentry vehicle subject to bounded uncertainty. A new continuous adaptive super-twisting sliding mode control (ASTSMC) method is developed based on conventional super-twisting sliding mode control (STSMC) and adaptive gain technique, which can improve tracking accuracy and achieve high control performance. Based on adaptive gain technique, the designed ASTSMC method requires no prior information on uncertainty and avoids the overestimation of control gain, then the unexpected chattering phenomenon is alleviated. By employing fast power rate reaching law and modified fast nonsingular terminal sliding mode (FNTSM) surface, the designed controller achieves faster convergence and stronger robustness than conventional STSMC methods. Furthermore, the finite-time stability of closed-loop system is proved through Lyapunov theory. Simulation results are executed to validate the superiority of the proposed controller.
Author Shen, Ganghui
Xia, Yuanqing
Zhang, Jinhui
Cui, Bing
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Keywords Finite-time control
Reentry vehicle
Super-twisting sliding mode control
Fast nonsingular terminal sliding mode
Adaptive law
Language English
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Snippet This paper addresses the altitude trajectory tracking control problem of reentry vehicle subject to bounded uncertainty. A new continuous adaptive...
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StartPage 329
SubjectTerms Adaptive law
Fast nonsingular terminal sliding mode
Finite-time control
Reentry vehicle
Super-twisting sliding mode control
Title Adaptive super-twisting sliding mode altitude trajectory tracking control for reentry vehicle
URI https://dx.doi.org/10.1016/j.isatra.2022.06.023
https://www.ncbi.nlm.nih.gov/pubmed/35798588
https://www.proquest.com/docview/2687719845
Volume 132
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