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JRM Vol.28 No.3 pp. 334-342
doi: 10.20965/jrm.2016.p0334
(2016)

Paper:

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Flight Characteristics of Quad Rotor Helicopter with Thrust Vectoring Equipment

Akitaka Imamura*, Masafumi Miwa**, and Junichi Hino**

*Osaka Sangyo University
3-1-1 Nakagaito, Daito, Osaka 574-8530, Japan

**Tokushima University
2-1 Minamijosanjima-cho, Tokushima 770-8506, Japan

Received:
September 26, 2015
Accepted:
March 21, 2016
Published:
June 20, 2016
Creative Commons License
Keywords:
quad rotor, UAV, ducted fan, extra thruster, tilting rotor
Abstract
A quad rotor helicopter (QRH) is a radio controlled (RC) aircraft that tilts its attitude to generate a horizontal force component to move in a certain direction. Using autonomous control, the attitude control system tilts the airframe against disturbances, such as wind. Thus, the attitude of a flying QRH is always slanted. In this study, three types of deflecting thruster were compared to maintain the position and horizontal attitude of the QRH. The extra thrusters are tilted to generate a thrust against disturbances without causing the airframe to incline. It is suitable for precise measurements for which the airframe posture should remain horizontal.
Thrust vectoring mechanisms for WRH

Thrust vectoring mechanisms for WRH

Cite this article as:
A. Imamura, M. Miwa, and J. Hino, “Flight Characteristics of Quad Rotor Helicopter with Thrust Vectoring Equipment,” J. Robot. Mechatron., Vol.28 No.3, pp. 334-342, 2016.
Data files:
References
  1. [1] M. Miwa, Y. Shigematsu, and T. Yamashita, “Control of ducted fan flying object using thrust vectoring,” J. Syst. Des. Dyn., Vol.6, No.3, pp. 322-334, 2012.
  2. [2] A. Imamura, S. Uemura, M. Miwa, and J. Hino, “Flight Characteristics of Quad Ducted Fan Helicopter with Thrust Vectoring Nozzles,” The J. of Unmanned System Technology, Vol.2, No.1, pp. 54-61, June 2014.
  3. [3] A. Imamura, Y. Urashiri, M. Miwa, and J. Hino, “Flight Characteristics of Quad Rotor Helicopter with Tilting Rotor,” The J. of Instrumentation, Automation and Systems, Vol.1, No.2, pp. 56-63, 2014.
  4. [4] A. Imamura, M. Miwa, and J. Hino, “Flight Characteristics of a Quadrotor Helicopter Using Extra Deflecting Thrusters,” The J. of Instrumentation, Automation and Systems, Vol.1, No.2, pp. 64-71, 2014.
  5. [5] J. Fleming and T. Jones, “Improving control system effectiveness for ducted fan VTOL UAVs operating in crosswinds,” 2nd AIAA “Unmanned Unlimited” Conf. and Workshop & Exhibit, 2003-6514, 2003.
  6. [6] M. Kumon, H. Cover, and J. Katupitiya, “Hovering Control of Vectored Thrust Aerial Vehicles,” IEEE Int. Conf. on Robotics and Automation, pp. 1149-1154, 2010.
  7. [7] W. Shuai and Q. Xiao-hui, “Aerodynamic Data Model Analysis and Simulation of Ducted Fan UAV,” 2011 Int. Conf. on Electronics, Communications, and Control (ICECC), pp. 699-702, 2011.
  8. [8] J. Gebauer and P. Koci, “Measurements of Features of the Ducted Fan as a Possible Actuator of a Multi-copter Vehicle,” 2011 12th Int. Carpathian Control Conf. (ICCC), pp. 127-130, 2011.
  9. [9] M. Ryll, H. H. Bülthoff, and P. R. Giordano, “Modeling and control of a quad rotor UAV with tilting propellers,” IEEE Int. Conf. on Robotics and Automation, pp. 4606-4613, 2012.
  10. [10] M. Ryll, H. H. Bülthoff, and P. R. Giordano, “First Flight Tests for a Quadrotor UAV with Tilting Propellers,” IEEE Int. Conf. on Robotics and Automation, pp. 295-302, 2013.
  11. [11] P. Segui-Gasco, Y. Al-Rihani, S. Hyo-Sang, and A. Savvaris, “A novel actuation concept for a multi rotor UAV,” IEEE Int. Conf. on Unmanned Aircraft Systems, pp. 373-382, 2013.

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Last updated on Oct. 11, 2024