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    Dynamic Tube Model Predictive Control for Powered-Descent Guidance

    Source: Journal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 006::page 04022098
    Author:
    Long Cheng
    ,
    Hao Wen
    ,
    Junjie Kang
    ,
    Dongping Jin
    DOI: 10.1061/(ASCE)AS.1943-5525.0001487
    Publisher: ASCE
    Abstract: In this paper, a dynamic tube nonlinear model predictive control (NMPC) scheme is developed to solve the powered-descent guidance (PDG) problem in the presence of bounded disturbances and no-fly zones. First, owing to its simplicity and robustness, time-varying boundary layer sliding mode control (SMC) is used as an ancillary controller to compensate for external disturbances. Consequently, the tube geometry dynamics can be established as first-order differential equations to calculate the robust control invariant tube. Hence, the nominal trajectory and tube geometry are optimized simultaneously to improve the control performance by augmenting the tube geometry dynamics in open-loop MPC optimization. Moreover, the tube can be shrunk to reduce the conservativeness and enhance optimization feasibility by exploiting the tube geometry and tracking error dynamics. In addition, a constraint-tightening method is employed to ensure that the PDG problem satisfies all the constraints while accounting for the uncertainty caused by the disturbance. Finally, numerical case studies and Monte Carlo simulations validate the effectiveness and performance of the proposed strategy.
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      Dynamic Tube Model Predictive Control for Powered-Descent Guidance

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4289538
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    • Journal of Aerospace Engineering

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    contributor authorLong Cheng
    contributor authorHao Wen
    contributor authorJunjie Kang
    contributor authorDongping Jin
    date accessioned2023-04-07T00:40:56Z
    date available2023-04-07T00:40:56Z
    date issued2022/11/01
    identifier other%28ASCE%29AS.1943-5525.0001487.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4289538
    description abstractIn this paper, a dynamic tube nonlinear model predictive control (NMPC) scheme is developed to solve the powered-descent guidance (PDG) problem in the presence of bounded disturbances and no-fly zones. First, owing to its simplicity and robustness, time-varying boundary layer sliding mode control (SMC) is used as an ancillary controller to compensate for external disturbances. Consequently, the tube geometry dynamics can be established as first-order differential equations to calculate the robust control invariant tube. Hence, the nominal trajectory and tube geometry are optimized simultaneously to improve the control performance by augmenting the tube geometry dynamics in open-loop MPC optimization. Moreover, the tube can be shrunk to reduce the conservativeness and enhance optimization feasibility by exploiting the tube geometry and tracking error dynamics. In addition, a constraint-tightening method is employed to ensure that the PDG problem satisfies all the constraints while accounting for the uncertainty caused by the disturbance. Finally, numerical case studies and Monte Carlo simulations validate the effectiveness and performance of the proposed strategy.
    publisherASCE
    titleDynamic Tube Model Predictive Control for Powered-Descent Guidance
    typeJournal Article
    journal volume35
    journal issue6
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0001487
    journal fristpage04022098
    journal lastpage04022098_10
    page10
    treeJournal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 006
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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