Towards Long-endurance Flight: Design and Implementation of a Variable-pitch Gasoline-engine Quadrotor

Pang, Tao; Peng, Kaile; Lin, Feng; Chen, B. M.

doi:10.48550/arxiv.1708.02922

2017

DOI: 10.48550/arxiv.1708.02922

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Towards Long-endurance Flight: Design and Implementation of a Variable-pitch Gasoline-engine Quadrotor

Tao Pang¹,

Kaile Peng²,

Feng Lin³

et al.

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2018

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Control System Design and Experimental Validation of Hybrid Multicopter for Endurance Enhancement

2018

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In this paper, We propose a hybrid multicopter that combines an gasoline propulsion system and an electric propulsion system to improve the endurance of the multicopter. The hybrid is equipped with a coaxial inverting thruster using a gasoline engine at the center and an electric propulsion system for attitude control at the side. The control system using a classical control algorithm based on the dynamic model. Finally, flight performance and high-endurance flight of the hybrid multicopter were verified. Keywords:We would like to encourage you to list your keywords in this section.

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Control System Design and Experimental Validation of Hybrid Multicopter for Endurance Enhancement

2018

AJMSM

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Towards Long-endurance Flight: Design and Implementation of a Variable-pitch Gasoline-engine Quadrotor

Cited by 1 publication

References 2 publications

Control System Design and Experimental Validation of Hybrid Multicopter for Endurance Enhancement

Control System Design and Experimental Validation of Hybrid Multicopter for Endurance Enhancement

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