1. Date of download: 11/11/2017
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From: Modeling of Cross-Coupling Responses on Hingeless Helicopters via Gyroscopic Effect
J. Comput. Nonlinear Dynam. 2012;7(2): doi: /
Figure Legend:
Using the analytical forms (4), (6), and (3), this figure plots the variation of the cyclic pitch angles of a main blade in a function of the azimuth angle. The control commands are recorded from a commercially available R/C (remote control) transmitter (JR PCM9XII). Then, the collected input data goes into the derived analytical forms so as to obtain the resultant cyclic pitch angle at an azimuth angle.