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    Lambert’s Problem with Multiple Constraints

    Source: Journal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 005::page 04022066
    Author:
    Gang Zhang
    ,
    Huidong Ma
    ,
    Ming Liu
    DOI: 10.1061/(ASCE)AS.1943-5525.0001464
    Publisher: ASCE
    Abstract: This paper proposes a new method to solve Lambert’s problem with multiple constraints, including the impulse-magnitude constraints, the trajectory-radius constraints, and the terminal-impact-angle constraint. First, the closed-form range of the chordal terminal velocity component for each constraint is derived. Then, the admissible intersection range for all constraints is obtained. Finally, the feasible solutions are solved in the admissible intersection range by using the terminal-velocity-based Lambert algorithm. The 180° case and the multiple-revolution case are also considered. The proposed method can be also extended to the Lambert algorithms with other independent variables. Compared with the typical method of first solving Lambert’s problem and then pruning the solutions that do not satisfy the constraints, the numerical examples show that the proposed method can reduce a lot of computational time.
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      Lambert’s Problem with Multiple Constraints

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4286387
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    contributor authorGang Zhang
    contributor authorHuidong Ma
    contributor authorMing Liu
    date accessioned2022-08-18T12:18:13Z
    date available2022-08-18T12:18:13Z
    date issued2022/06/09
    identifier other%28ASCE%29AS.1943-5525.0001464.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4286387
    description abstractThis paper proposes a new method to solve Lambert’s problem with multiple constraints, including the impulse-magnitude constraints, the trajectory-radius constraints, and the terminal-impact-angle constraint. First, the closed-form range of the chordal terminal velocity component for each constraint is derived. Then, the admissible intersection range for all constraints is obtained. Finally, the feasible solutions are solved in the admissible intersection range by using the terminal-velocity-based Lambert algorithm. The 180° case and the multiple-revolution case are also considered. The proposed method can be also extended to the Lambert algorithms with other independent variables. Compared with the typical method of first solving Lambert’s problem and then pruning the solutions that do not satisfy the constraints, the numerical examples show that the proposed method can reduce a lot of computational time.
    publisherASCE
    titleLambert’s Problem with Multiple Constraints
    typeJournal Article
    journal volume35
    journal issue5
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0001464
    journal fristpage04022066
    journal lastpage04022066-9
    page9
    treeJournal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 005
    contenttypeFulltext
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    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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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
    yabeshDSpacePersian