YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASME
    • Journal of Mechanisms and Robotics
    • View Item
    •   YE&T Library
    • ASME
    • Journal of Mechanisms and Robotics
    • View Item
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Archive

    Origami-Inspired Collapsible Structures for Small Rotorcraft Collision Resilience and Landing

    Source: Journal of Mechanisms and Robotics:;2024:;volume( 017 ):;issue: 004::page 44506-1
    Author:
    Chang, Andrew L.
    ,
    Munoz, Ivonne
    ,
    Sanchez, Christopher
    ,
    Sanchez IV, Leopoldo
    ,
    Lee, Christopher L.
    DOI: 10.1115/1.4066925
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This article reports on the design, fabrication, and testing of flexible, collapsible structures inspired by origami and kirigami that can be used to protect small rotorcraft from collision impacts and to serve as landing gear. Twenty structures created from variations of Pako Pako, Magic Ball, and Herringbone fold patterns were laser cut from cardstock and evaluated experimentally. Some of the Pako Pako structures were designed to have graduated mechanical stiffness. An empirical procedure based on acceleration measurements has been developed that enables quantitative evaluation of each structure based on the characterization parameters of peak acceleration, peak velocity, translational kinetic energy, impact duration, mass, and mechanical stiffness. Structures were mounted onto the front of a radio-controlled (RC) car and driven on a linear test track into a rigid wall. Accelerations measured during the collisions were numerically integrated to determine velocities over the impact and collapse/compression of the structures. Flight tests conducted with small RC quadcopters demonstrated that the collapsible structures could successfully be used to mitigate collisions, enough to enable the quadcopters to continue flying after a direct impact and to land indoors or on outdoor terrain with varying slopes and surfaces. Based on trade-off comparisons between the evaluative metrics of the cases studied, conical Pako Pako structures with uniform stiffness are shown to be the most effective for collision resilience and landing.
    • Download: (1.678Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      Origami-Inspired Collapsible Structures for Small Rotorcraft Collision Resilience and Landing

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4308366
    Collections
    • Journal of Mechanisms and Robotics

    Show full item record

    contributor authorChang, Andrew L.
    contributor authorMunoz, Ivonne
    contributor authorSanchez, Christopher
    contributor authorSanchez IV, Leopoldo
    contributor authorLee, Christopher L.
    date accessioned2025-08-20T09:29:24Z
    date available2025-08-20T09:29:24Z
    date copyright11/6/2024 12:00:00 AM
    date issued2024
    identifier issn1942-4302
    identifier otherjmr_17_4_044506.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4308366
    description abstractThis article reports on the design, fabrication, and testing of flexible, collapsible structures inspired by origami and kirigami that can be used to protect small rotorcraft from collision impacts and to serve as landing gear. Twenty structures created from variations of Pako Pako, Magic Ball, and Herringbone fold patterns were laser cut from cardstock and evaluated experimentally. Some of the Pako Pako structures were designed to have graduated mechanical stiffness. An empirical procedure based on acceleration measurements has been developed that enables quantitative evaluation of each structure based on the characterization parameters of peak acceleration, peak velocity, translational kinetic energy, impact duration, mass, and mechanical stiffness. Structures were mounted onto the front of a radio-controlled (RC) car and driven on a linear test track into a rigid wall. Accelerations measured during the collisions were numerically integrated to determine velocities over the impact and collapse/compression of the structures. Flight tests conducted with small RC quadcopters demonstrated that the collapsible structures could successfully be used to mitigate collisions, enough to enable the quadcopters to continue flying after a direct impact and to land indoors or on outdoor terrain with varying slopes and surfaces. Based on trade-off comparisons between the evaluative metrics of the cases studied, conical Pako Pako structures with uniform stiffness are shown to be the most effective for collision resilience and landing.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOrigami-Inspired Collapsible Structures for Small Rotorcraft Collision Resilience and Landing
    typeJournal Paper
    journal volume17
    journal issue4
    journal titleJournal of Mechanisms and Robotics
    identifier doi10.1115/1.4066925
    journal fristpage44506-1
    journal lastpage44506-9
    page9
    treeJournal of Mechanisms and Robotics:;2024:;volume( 017 ):;issue: 004
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian