Parameter effect on the novel swashplateless rotor control

Author:

Tang Linkai1ORCID,Chang Min1ORCID,Huang Yaping1,Zu Siliang2,Bai Junqiang1

Affiliation:

1. Unmanned System Research Institute, Northwestern Polytechnical University, Xi’an, China

2. School of Astronautics, Northwestern Polytechnical University, Xi’an, China

Abstract

To achieve underactuated control, a novel swashplateless rotor configuration of asymmetric inclined hinges which can be driven by periodic sinusoidal torque is studied, hopefully eliminating the conventional swashplate mechanism and multiple actuators. Therefore, the traditional mechanism can be intelligently replaced by software. However, high-frequency torque variation will invariably result in vibration noise and energy loss.Thus it is critical to properly design the swashplateless rotor in order to achieve a control process with less torque variation. As a result, in both numerical simulation and experiments, we performed sensitivity analyses on related design parameters such as hinge eccentricity, hinge inclined angle, and wingtip hammer position. The parameter effect on swashplateless rotor control was discovered through the analyses, and the basic law of its design was obtained.

Funder

Youth Innovation Promotion Association CAS

National Natural Science Foundation of China

Publisher

SAGE Publications

Reference9 articles.

1. Fujihara Y, Ando M. Device for inclining the tip path plane of a propeller of toy helicopter, 1992. US Patent 5,110,314.

2. Reich S. Drehflügler, rotorsystem und steuerung, 2005. WO2005087587A1.

3. An underactuated propeller for attitude control in micro air vehicles

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1. Characterization of different hinge angles for swashplateless micro aerial robots;Engineering Science and Technology, an International Journal;2024-07

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