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2017 | OriginalPaper | Chapter

3. Airframe Design

Author : Quan Quan

Published in: Introduction to Multicopter Design and Control

Publisher: Springer Singapore

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Abstract

When given a multicopter, its configuration and structure come into our sight first, including the shape and size of the airframe, the choice of motors and propellers, and the distribution of the battery and the payload.

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Footnotes
1
The ultimate payload is the limit payload multiplied by prescribed factors of safety. For example, a factor of safety of 1.5 can be used.
 
2
The ability of a material to absorb energy and plastically deform without fracturing.
 
Literature
1.
go back to reference Bohorquez F (2007) Rotor hover performance and system design of an efficient coaxial rotary wing micro air vehicle. Dissertation, University of Maryland College Park Bohorquez F (2007) Rotor hover performance and system design of an efficient coaxial rotary wing micro air vehicle. Dissertation, University of Maryland College Park
2.
go back to reference Ryll M, Bulthoff HH, Giordano PR (2015) A novel overactuated quadrotor unmanned aerial vehicle: modeling, control, and experimental validation. IEEE Trans Control Syst Technol 23(2):540–556 Ryll M, Bulthoff HH, Giordano PR (2015) A novel overactuated quadrotor unmanned aerial vehicle: modeling, control, and experimental validation. IEEE Trans Control Syst Technol 23(2):540–556
3.
go back to reference Hwang JY, Jung MK, Kwon OJ (2014) Numerical study of aerodynamic performance of a multirotor unmanned-aerial-vehicle configuration. J Aircr 52(3):839–846CrossRef Hwang JY, Jung MK, Kwon OJ (2014) Numerical study of aerodynamic performance of a multirotor unmanned-aerial-vehicle configuration. J Aircr 52(3):839–846CrossRef
4.
go back to reference Harrington AM (2011) Optimal propulsion system design for a micro quadrotor. Dissertation, University of Maryland College Park Harrington AM (2011) Optimal propulsion system design for a micro quadrotor. Dissertation, University of Maryland College Park
5.
go back to reference Mahony R, Kumar V, Corke P (2012) Multirotor aerial vehicles: modeling, estimation, and control of quadrotor. IEEE Robot Autom Mag 19(3):20–32CrossRef Mahony R, Kumar V, Corke P (2012) Multirotor aerial vehicles: modeling, estimation, and control of quadrotor. IEEE Robot Autom Mag 19(3):20–32CrossRef
6.
go back to reference White FM (1999) Fluid mechanics. McGraw-Hill, New York White FM (1999) Fluid mechanics. McGraw-Hill, New York
7.
go back to reference Bristeau PJ, Martin P, Salaun E et al (2009) The role of propeller aerodynamics in the model of a quadrotor UAV. In: European control conference (ECC), Budapest, August, pp 683–688 Bristeau PJ, Martin P, Salaun E et al (2009) The role of propeller aerodynamics in the model of a quadrotor UAV. In: European control conference (ECC), Budapest, August, pp 683–688
8.
go back to reference Pounds P, Mahony R, Corke P (2010) Modelling and control of a large quadrotor robot. Control Eng Pract 18(7):691–699CrossRef Pounds P, Mahony R, Corke P (2010) Modelling and control of a large quadrotor robot. Control Eng Pract 18(7):691–699CrossRef
10.
go back to reference Thomas ASW (1984) Aircraft drag reduction technology. Lockheed-Georgia Co Marietta Flight Sciences Div Thomas ASW (1984) Aircraft drag reduction technology. Lockheed-Georgia Co Marietta Flight Sciences Div
12.
go back to reference Marte JE, Kurtz DW (1970) A review of aerodynamic noise from propellers, rotors and lift fans. Technical report 32–1462, Jet Propulsion Laboratory, California Institute of Technology, USA Marte JE, Kurtz DW (1970) A review of aerodynamic noise from propellers, rotors and lift fans. Technical report 32–1462, Jet Propulsion Laboratory, California Institute of Technology, USA
13.
go back to reference Harper-Bourne M (1972) Model turbojet exhaust noise part 2. contract report no CR72/31. Institute of sound and vibration research, University of Southampton, Southampton Harper-Bourne M (1972) Model turbojet exhaust noise part 2. contract report no CR72/31. Institute of sound and vibration research, University of Southampton, Southampton
14.
go back to reference Beckman BC (2016) Vehicle noise control and communication. US patent 20,160,083,073 Beckman BC (2016) Vehicle noise control and communication. US patent 20,160,083,073
Metadata
Title
Airframe Design
Author
Quan Quan
Copyright Year
2017
Publisher
Springer Singapore
DOI
https://doi.org/10.1007/978-981-10-3382-7_3