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    Bank-to-Turn Guidance Law with Terminal Impact-Angle Constraint

    Source: Journal of Aerospace Engineering:;2016:;Volume ( 029 ):;issue: 003
    Author:
    Wen Qiuqiu
    ,
    Xia Qunli
    ,
    Su Weixia
    DOI: 10.1061/(ASCE)AS.1943-5525.0000552
    Publisher: American Society of Civil Engineers
    Abstract: To avoid the mathematical singularity of polar converting in bank-to-turn (BTT) guidance and to provide the specified terminal impact angle, a BTT guidance law with impact-angle constraint (BTT-GL/IA) is presented. Considering the influence of the impact-angle control and target maneuver to the miss-distance, a new form zero-effort miss-distance with impact angle (ZEM/IA) is introduced. Referring to the Lyapunov-like approach used to drive the guidance law in the prior literature, a Lyapunov function is constructed in terms of ZEM/IA. Based on the Lyapunov stability theorem, a negative definite function is designed, and the BTT-GL/IA is derived. Next, BTT-GL/IA is implemented in another form with the variables as the line-of-sight angle and its rate, which are easily measured by the seeker. When using BTT-GL/IA, the guidance law tends to maintain smooth and continuously-varied body acceleration and roll-angle commands while satisfying the impact position and angle constraints. The problem of a mathematical singularity in normal BTT polar converting logic is avoided. Finally, both the maneuverable and stationary targets with different impact-angle constraints are considered in numerical simulations. Through various simulation results, the effectiveness and practicality of the BTT-GL/IA are demonstrated.
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      Bank-to-Turn Guidance Law with Terminal Impact-Angle Constraint

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    https://yetl.yabesh.ir/yetl1/handle/yetl/4242122
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    • Journal of Aerospace Engineering

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    contributor authorWen Qiuqiu
    contributor authorXia Qunli
    contributor authorSu Weixia
    date accessioned2017-12-16T09:22:50Z
    date available2017-12-16T09:22:50Z
    date issued2016
    identifier other%28ASCE%29AS.1943-5525.0000552.pdf
    identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4242122
    description abstractTo avoid the mathematical singularity of polar converting in bank-to-turn (BTT) guidance and to provide the specified terminal impact angle, a BTT guidance law with impact-angle constraint (BTT-GL/IA) is presented. Considering the influence of the impact-angle control and target maneuver to the miss-distance, a new form zero-effort miss-distance with impact angle (ZEM/IA) is introduced. Referring to the Lyapunov-like approach used to drive the guidance law in the prior literature, a Lyapunov function is constructed in terms of ZEM/IA. Based on the Lyapunov stability theorem, a negative definite function is designed, and the BTT-GL/IA is derived. Next, BTT-GL/IA is implemented in another form with the variables as the line-of-sight angle and its rate, which are easily measured by the seeker. When using BTT-GL/IA, the guidance law tends to maintain smooth and continuously-varied body acceleration and roll-angle commands while satisfying the impact position and angle constraints. The problem of a mathematical singularity in normal BTT polar converting logic is avoided. Finally, both the maneuverable and stationary targets with different impact-angle constraints are considered in numerical simulations. Through various simulation results, the effectiveness and practicality of the BTT-GL/IA are demonstrated.
    publisherAmerican Society of Civil Engineers
    titleBank-to-Turn Guidance Law with Terminal Impact-Angle Constraint
    typeJournal Paper
    journal volume29
    journal issue3
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000552
    treeJournal of Aerospace Engineering:;2016:;Volume ( 029 ):;issue: 003
    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
    yabeshDSpacePersian