
In this paper a simplified model and a nonlinear control algorithm for a coaxial helicopter are presented. The model of the helicopter dynamics is obtained in hover conditions. By neglecting the small body forces due to the mechanism used to obtain the torque control, a dynamic controller, based on backstepping techniques, is developed. Some simulation results are presented to illustrate the performance of such a controller.
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| popularity This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network. | Average | |
| influence This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically). | Top 10% | |
| impulse This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network. | Average |
