Stability Flight Control and Verification on Hybrid Powered Multi-Rotor System

  • 莊 凱堤

Student thesis: Master's Thesis

Abstract

The development of multi-rotor system has been improved and applied to various applications However with constraints on battery and motor the performance of multi-rotor system is limited in payload and flight endurance The limitations are solved by introducing gas engine to work with DC brushless motor 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 System design considerations on high thrust reverse torque vibration structure and weight balance are included by carefully weight reduction into fabrication Microprocessor control system is designed and implemented to make gas engine control speed precisely in both directions Two practical flight tests have completed on this dual quad-rotor system to verify its stability flight control and payload capability
Date of Award2016 Aug 15
Original languageEnglish
SupervisorChin-E. Lin (Supervisor)

Cite this

Stability Flight Control and Verification on Hybrid Powered Multi-Rotor System
凱堤, 莊. (Author). 2016 Aug 15

Student thesis: Master's Thesis