In the last five years, advances in materials, electronics, sensors, and batteries have fueled a growth in the development of microunmanned aerial vehicles (MAVs) that are between 0.1 and 0.5 m in length and 0.1-0.5 kg in mass (1). A few groups have built and analyzed MAVs in the 10-cm range (2), (3). One of the smallest MAV is the Picoftyer with a 60-mmpropellor diameter and a mass of 3.3 g (4). Platforms in the 50-cm range are more prevalent with several groups having built and flown systems of this size (5)-(7). In fact, there are severalcommercially available radiocontrolled (PvC) helicopters and research-grade helicopters in this size range (8).


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    Titel :

    The GRASP Multiple Micro-UAV Testbed


    Beteiligte:
    Michael, N. (Autor:in) / Mellinger, D. (Autor:in) / Lindsey, Q. (Autor:in) / Kumar, V. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2010


    Format / Umfang :

    10 Seiten, 19 Quellen




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch





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