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Fluid dynamics / Stall / Control theory / Gliding flight / Elevator / Angle of attack / Drag / Glider / Model aircraft / Aerospace engineering / Aerodynamics / Aviation


Experiments in Fixed-Wing UAV Perching Rick Cory∗ and Russ Tedrake† MIT Computer Science and Artificial Intelligence Lab, Cambridge, MA, 02139, USA High-precision maneuvers at high angles-of-attack are not properly a
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Document Date: 2008-08-19 23:12:52


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File Size: 2,36 MB

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City

Cambridge / /

Company

NEC / /

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Facility

American Institute of Aeronautics / /

IndustryTerm

acrobatic control systems / machine learning control technology / real-time hardware interface communicating new state information / offline control policy search algorithm / energy input / aircraft control systems / control solutions / closed-form solutions / control systems / less energy / decrease energy / control policy search algorithm / real-time tracking software locks / /

NaturalFeature

Full River / /

OperatingSystem

Linux / /

Organization

American Institute of Aeronautics and Astronautics V / American Institute of Aeronautics and Astronautics / American Institute of Aeronautics / MIT / Cornell / American Institute of Aeronautics and Astronautics Figure / Tedrake† MIT Computer Science and Artificial Intelligence Lab / /

Person

Jim Holzberger / John Roberts / Zack Jackowski / Russ Tedrake / /

Position

simple controller / pilot control data / Professor / representative / forward / Assistant / controller / /

Product

dihedral / /

ProvinceOrState

Massachusetts / /

Technology

ethernet / laser / control policy search algorithm / offline control policy search algorithm / Linux / fluid dynamics / machine learning / simulation / machine learning control technology / /

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