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Lighter than Air RobotsModeling

Lighter than Air Robots: Modeling [Nowadays, non rigid airships with a cigar shaped profile are the most common type. These airships do not have any rigid internal framework. The objective of this chapter is to present kinematics and dynamics models of a lighter than air robot, taking into account wind effect. Newton-Euler and Hamilton-Lagrange approaches are used for this discussion then the translational model is presented. Here, motion is referenced to a system of orthogonal body axes fixed in the airship, with the origin assumed to coincide with the bow. Finally, some aerology characteristics are briefly discussed.] http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png

Lighter than Air RobotsModeling

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Publisher
Springer Netherlands
Copyright
© Springer Science+Business Media B.V. 2012
ISBN
978-94-007-2662-8
Pages
7 –44
DOI
10.1007/978-94-007-2663-5_2
Publisher site
See Chapter on Publisher Site

Abstract

[Nowadays, non rigid airships with a cigar shaped profile are the most common type. These airships do not have any rigid internal framework. The objective of this chapter is to present kinematics and dynamics models of a lighter than air robot, taking into account wind effect. Newton-Euler and Hamilton-Lagrange approaches are used for this discussion then the translational model is presented. Here, motion is referenced to a system of orthogonal body axes fixed in the airship, with the origin assumed to coincide with the bow. Finally, some aerology characteristics are briefly discussed.]

Published: Sep 6, 2011

Keywords: Ring Vortex; Lift Force; Euler Angle; Aerodynamic Force; Aerodynamic Lift

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