DocumentCode :
1319496
Title :
The GRASP Multiple Micro-UAV Testbed
Author :
Michael, Nathan ; Mellinger, Daniel ; Lindsey, Quentin ; Kumar, Vijay
Author_Institution :
Mech. Eng., Univ. of Pennsylvania, Philadelphia, PA, USA
Volume :
17
Issue :
3
fYear :
2010
Firstpage :
56
Lastpage :
65
Abstract :
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].
Keywords :
aerospace control; helicopters; mobile robots; remotely operated vehicles; GRASP; MAV; flown systems; microunmanned aerial vehicles; multiple micro-UAV testbed; research grade helicopters; Acceleration; Mathematical model; Robot kinematics; Rotors; Software; Trajectory; Unmanned aerial vehicles;
fLanguage :
English
Journal_Title :
Robotics & Automation Magazine, IEEE
Publisher :
ieee
ISSN :
1070-9932
Type :
jour
DOI :
10.1109/MRA.2010.937855
Filename :
5569026
Link To Document :
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