Dynamic Simulation of an Unmanned Hybrid Flying Robot-Reference-Cited by-同舟云学术

Dynamic Simulation of an Unmanned Hybrid Flying Robot

Published:2015-09 Issue:3 Volume:7 Page:257-273
ISSN:1756-8293
Container-title:International Journal of Micro Air Vehicles
language:en
Short-container-title:International Journal of Micro Air Vehicles

Author:

Alsaif khalid A.¹,Foda Mosaad A.²,Rosyid Abdur³

Affiliation:

1. Department of Mechanical Engineering, King Saud University, and King Abdulaziz City for Science and Technology, Riyadh 11421, Saudi Arabia

2. Department of Production Engineering and Mechanical Design, Mansoura University, Gmhouria St., Mansoura 35516, Egypt

3. Department of Mechanical Engineering, King Saud University, Riyadh 11421, Saudi Arabia

Abstract

This paper considers the dynamic simulation of an Unmanned Hybrid Flying Robot (UHFR) with main fuel engine in the middle to carry most of the weight and promises long flights. This configuration will increase the flight time of the unmanned copter for a given payload size as opposed to the traditional quad-copters, where only DC motors are used. A parametric study to investigate the effect of the propellers ratio (main rotor propeller diameter to secondary rotor propeller diameter), the angle of incidence of the main rotor and the twist angle of the main rotor blades on selected performance criteria of the UHFR is presented.

Publisher

SAGE Publications

Subject

Aerospace Engineering

Link

http://journals.sagepub.com/doi/pdf/10.1260/1756-8293.7.3.257

Reference19 articles.

1. Estimation and Control of a Quadrotor Vehicle Using Monocular Vision and Moiré Patterns

2. Imaging from an unmanned aerial vehicle: agricultural surveillance and decision support

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