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    A Novel Control Surface for Energy-Optimum Maneuver for Solar-Powered Aircraft

    Source: Journal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 001::page 04023099-1
    Author:
    Vijay Shankar Dwivedi
    ,
    A. K. Ghosh
    ,
    G. M. Kamath
    DOI: 10.1061/JAEEEZ.ASENG-4987
    Publisher: ASCE
    Abstract: This paper presents a new control surface, which we have named auxiron, that helps a solar-powered aircraft to orient itself according to the position of the sun in the sky to collect more solar power. The auxiron also enables an aircraft to land in crosswind conditions with no or reduced sideslip angle depending on the auxiron control power. The auxiron serves to produce the necessary side aerodynamic force for counterbalancing the horizontal component of the lift force. Its primary purpose is to eliminate the sideslip angle during flight with a nonzero bank angle. This results in a reduction in aerodynamic drag and power consumption required to maintain a straight-line flight with nonzero bank angles. By implementing this innovative control surface, an aircraft can now cruise straight without experiencing any sideslip angle, even with nonzero bank angles. The modified stability and control derivatives for the aircraft configuration with the auxiron are established, and these derivatives are incorporated into the aircraft dynamics. The 6-DoF simulation is carried out for the solar UAV, Maraal, which demonstrates the effectiveness of the auxiron.
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      A Novel Control Surface for Energy-Optimum Maneuver for Solar-Powered Aircraft

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4297166
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    • Journal of Aerospace Engineering

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    contributor authorVijay Shankar Dwivedi
    contributor authorA. K. Ghosh
    contributor authorG. M. Kamath
    date accessioned2024-04-27T22:39:00Z
    date available2024-04-27T22:39:00Z
    date issued2024/01/01
    identifier other10.1061-JAEEEZ.ASENG-4987.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4297166
    description abstractThis paper presents a new control surface, which we have named auxiron, that helps a solar-powered aircraft to orient itself according to the position of the sun in the sky to collect more solar power. The auxiron also enables an aircraft to land in crosswind conditions with no or reduced sideslip angle depending on the auxiron control power. The auxiron serves to produce the necessary side aerodynamic force for counterbalancing the horizontal component of the lift force. Its primary purpose is to eliminate the sideslip angle during flight with a nonzero bank angle. This results in a reduction in aerodynamic drag and power consumption required to maintain a straight-line flight with nonzero bank angles. By implementing this innovative control surface, an aircraft can now cruise straight without experiencing any sideslip angle, even with nonzero bank angles. The modified stability and control derivatives for the aircraft configuration with the auxiron are established, and these derivatives are incorporated into the aircraft dynamics. The 6-DoF simulation is carried out for the solar UAV, Maraal, which demonstrates the effectiveness of the auxiron.
    publisherASCE
    titleA Novel Control Surface for Energy-Optimum Maneuver for Solar-Powered Aircraft
    typeJournal Article
    journal volume37
    journal issue1
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/JAEEEZ.ASENG-4987
    journal fristpage04023099-1
    journal lastpage04023099-9
    page9
    treeJournal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 001
    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