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    Specialized Algorithm for Navigation of a Micro Hopping Air Vehicle Using Only Inertial Sensors 

    Source: Journal of Dynamic Systems, Measurement, and Control:;2013:;volume( 135 ):;issue: 002:;page 24505
    Author(s): Scheuermann, Edward; Costello, Mark
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The need for accurate and reliable navigation techniques for micro air vehicles plays an important part in enabling autonomous operation. Traditional navigation systems typically rely on periodic global positioning system ...
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    Rotorcraft Robotic Landing Gear With Locking Mechanisms 

    Source: Journal of Dynamic Systems, Measurement, and Control:;2023:;volume( 145 ):;issue: 006:;page 61002-1
    Author(s): Kim, Dooroo; Butler, Cason; Costello, Mark
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Robotic landing gear (RLG) for rotorcraft improves performance in landing on sloped uneven terrain, unprepared areas, and ship decks. The interaction between the feet of the RLG and the landing surface are pivotal to a ...
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    Global Positioning System Denied Navigation of Autonomous Parafoil Systems Using Beacon Measurements From a Single Location 

    Source: Journal of Dynamic Systems, Measurement, and Control:;2018:;volume( 140 ):;issue: 004:;page 41004
    Author(s): Cacan, Martin R.; Costello, Mark; Scheuermann, Edward
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Precision-guided airdrop systems have shown considerable accuracy improvements over more widely used unguided systems through high-quality position, velocity, and time feedback provided by global positioning system (GPS). ...
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    Actuator Design and Flight Testing of an Active Microspoiler-Equipped Projectile 

    Source: Journal of Dynamic Systems, Measurement, and Control:;2017:;volume( 139 ):;issue: 011:;page 111002
    Author(s): Kim, Dooroo; Strickland, Laura; Gross, Matthew; Rogers, Jonathan; Costello, Mark; Fresconi, Frank; Celmins, Ilmars
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Actively controlled gun-launched projectiles require a means of modifying the projectile flight trajectory. While numerous potential mechanisms exist, microspoiler devices have been shown to be a promising control actuator ...
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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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