Engine controller system of hybrid powered multi-rotor system

Chin E. Lin, Kai Ti Jhuang, Thanakorn Supsukbaworn

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

To overcome the limitations of payload and flight endurance, a hybrid powered multi-rotor system is designed by dual systems which include engine-driven quad-rotor and motor-driven quadrotor. The proposed multi-rotor system is named Quad-in-Quad (QiQ) system. Since the characteristic of high thrust, engine takes in charge of major lift of the system. To provide stable lift, microprocessor control system is designed and implemented to make gas engine control speed precisely in both directions. Linearization of input and output makes engine be controlled with PID controller. And step response tests have completed on engines to achieve the precise RPM control and similar characteristics of four engines, which helps the stability flight control of the system.

Original languageEnglish
Title of host publication2016 International Automatic Control Conference, CACS 2016
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages106-111
Number of pages6
ISBN (Electronic)9781509041084
DOIs
Publication statusPublished - 2017 Jul 10
Event2016 International Automatic Control Conference, CACS 2016 - Taichung, Taiwan
Duration: 2016 Nov 92016 Nov 11

Publication series

Name2016 International Automatic Control Conference, CACS 2016

Other

Other2016 International Automatic Control Conference, CACS 2016
CountryTaiwan
CityTaichung
Period16-11-0916-11-11

All Science Journal Classification (ASJC) codes

  • Artificial Intelligence
  • Control and Systems Engineering
  • Control and Optimization

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