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Direction Controlled Descent of Samara Autorotating Wings (SAW) with N-Wings Research supported by the SUTD-MIT International Design Centre (IDC) and by the Temasek Laboratories Defence Innovation Research Programme (DIRP) IGDSP15020141
Conference proceeding

Direction Controlled Descent of Samara Autorotating Wings (SAW) with N-Wings Research supported by the SUTD-MIT International Design Centre (IDC) and by the Temasek Laboratories Defence Innovation Research Programme (DIRP) IGDSP15020141

Shane Kyi Hla Win, Tze Huan Goh, Jun En Low, Danial Sufiyan Bin Shaiful, Luke Thura Soe Win, Gim Song Soh and Shaohui Foong
The Institute of Electrical and Electronics Engineers, Inc. (IEEE) Conference Proceedings, p.6553
01/01/2018

Abstract

Autorotation Ball joints Computer simulation Control stability Controllability Defense programs Drop tests Gyroscopic stability Impact tests Laboratories Mathematical models Robotics Seeds Translational motion Wind tunnels
Conference Title: 2018 IEEE International Conference on Robotics and Automation (ICRA) Conference Start Date: 2018, May 21 Conference End Date: 2018, May 25 Conference Location: Brisbane, Australia The seeds of Maple trees (Samara) use autorotation as a unique mechanism to disperse their seeds. By exploiting gyroscopic stability of a spinning wing, the Samara is able to cover large horizontal distance despite having no form of propulsion. We applied and adapted this natural ability in our novel concept, the Samara Autorotating Wings (SAW), and extended its stability and direction controllability by generalizing the mechanism to incorporate designs with more than 1 wing. By conceiving cyclic control, the translational motion of autorotation is regulated. A nonlinear model of SAW with $n$ wings is derived and control schemes developed to control the translational position during autorotation. Numerical simulations were performed to investigate the performance of the multi-wing SAW prototypes to track a conical spiral autorotation trajectory. Direct experiments were conducted in a vertical wind-tunnel through a special ball joint that allows z-axis translation and all three rotational degrees of freedom. Finally, free-fall drop tests are used to verify the directional controllability and performance of SAW.

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