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研究生: 周明哲
Supsukbaworn, Thanakorn
論文名稱: 油電雙動力多旋翼機之設計與製造
Design and fabrication of Dual-Powered Gas Electric Multirotor
指導教授: 林清一
Lin, Chin-E
學位類別: 博士
Doctor
系所名稱: 工學院 - 航空太空工程學系
Department of Aeronautics & Astronautics
論文出版年: 2017
畢業學年度: 105
語文別: 英文
論文頁數: 101
外文關鍵詞: Multi-rotor system, quad-rotor in quad-rotor, high payload, long endurance, flight control and stability.
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  • The novel type of multi-rotor design is to enhance payload and endurance in performance over traditional electric multi-rotor. The bottleneck of battery defeats the multi-rotor endurance. A new idea to introduce internal combustion (IC) engine together with electric brushless DC (BLDC) motor to endurance multi-rotor system performance is proposed. Taking the advantage of energy density of gasoline being more than 40 times to Lithium Polymer (Li-Po) batteries, significant improvement over endurance and payload can be expected. The proposed multi-rotor designs an IC engine drive quad-rotor to provide main lift and work with a conventional LDC motor quad-rotor for attitude controls. Conceptually, it is a Quad-rotor-in-Quad-rotor (QiQ) Dual Powered multi-rotor system for improving endurance performance. The force moment dynamics of two quad-rotors is formulated to present main lift and control stability. Equal engine speed control strategy is implemented to stabilize high thrust control with an incremental PID controller. Noise reduction and vibration suppression are designed and fabricated into system integration. The flight control system including state estimation, sensor and actuator network and suitable controller is designed to realize the flight stabilization of the proposed QiQ design. System verification and flight demonstration show great improvement in system performance and flight stabilization. The QiQ multi-rotor concept is proven to be a solution from experiments to multi-rotor endurance and performance improvement.

    ABSTRACT I ACKNOWLEDGMENTS III CONTENTS IV LIST OF FIGURES VII LIST OF TABLES XII Chapter 1 Introduction 1 1.1 Overview & Research Background 1 1.2 Motivation 2 1.3 Significance of the problem 3 1.4 Problem statement 12 1.5 Scope and limitation of study 13 Chapter 2 Dual Power Multi-rotor Design Concept 14 2.1 Mechanical design 14 2.2 Mechanical design theory 14 2.3 Flight characteristics design 29 Chapter 3 Engine RPM stabilization system 38 3.1 Engine RPM stabilization design 38 3.2 Engine controller result 46 Chapter 4 State estimator design and implementation 54 4.1 Attitude filter design 54 4.2 Attitude filter result 58 4.3 Vertical estimator design 66 4.3.1 Altitude estimator 66 4.3.2 Vertical velocity estimator design 67 4.4 Vertical estimator result 70 4.5 Reference station effect in offset cancellation result 72 4.6 Vertical velocity estimation result 73 4.7 Real-time offset tracking result 75 Chapter 5 Flight stabilization system design 77 5.1 Attitude Stabilization 77 5.2 Attitude stabilization controller design 79 5.3 Attitude stabilization result 80 5.4 Altitude response performance experiments 83 5.5 Altitude control response performance experiments 87 Chapter 6 Conclusion 93 References 95

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