Abstract
This work shows first the way by which an inversion of the double linked fourbar has been obtained in order to use it as actuation mechanism for an UAV morphing wing after a short structural synthesis step. Then, the kinematical capabilities of this mechanism are outlined and graphically derived: instant center of rotation, lock positions and uncertainty positions. © Springer Science+Business Media Dordrecht 2013.
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CITATION STYLE
Aguirrebeitia, J., Aviĺes, R., De Bustos, I. F., & Abasolo, M. (2013). Kinematical capabilities of an inversion of the double linked fourbar for UAV morphingwing actuation. In Mechanisms and Machine Science (Vol. 7, pp. 3–11). Kluwer Academic Publishers. https://doi.org/10.1007/978-94-007-4902-3_1
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