Extra Thruster for Quad Rotor Helicopter
Abstract
of flying QRH always slants. In this study, extra thruster rotors are mountedto keep the position and horizontal attitude of QRH. Extra thrusters are tilted to generate thrust against to the disturbance without airframe inclination. This system is constructed with two ducted fans which can slant by two axes. To
oppose the crosswind, the thruster slants the ducted fan to leeward. Because the airframe is kept the horizontal, it is suitable for a precise measurement.
References
J. Shin, D. Fujiwara, K. Hazawa and K. Nonami, Model Based Optimal
Attitude and Positioning Control of Small-Scale Unmanned Helicopter,
Tran. Of the Japan Society of Mechanical Engineers, Vol.70, No.697
(2004), C, pp.2631-2637
S. Suzuki, D. Nakazwa, K. Nonami and M. Tawara, Attitude Control of
Small Electric Helicopter by Using Quaternion Feedback, Journal of
System Design and Dynamics, Vol.5, No.2 (2011), pp.231-247.
M. Miwa, I. Shiraishi, M. Matsushima and K. Minami, Remote Control
Support System for R/C Helicopter, ServiceRobotics and Mechatronics,
(2010), pp.125-130, Springer-Verlag
D. Pebrianti, F. Kendoul, S. Azrad, W. Wang and K. Nonami,
Autonomous Hovering and Landing of a Quad-rotor Micro Aerial
Vehicle by Means of on Ground Stereo Vision System, Journal of
System Design and Dynamics, Vol.4, No.2 (2010), pp.269-284.
M. Miwa, Y. Shigematsu, T. Yamashita," Control of Ducted Fan Flying
Object Using Thrust Vectoring," Journal of System Design and
Dynamics, Vol.6, No.3, pp.322-334, June 2012
DOI: http://dx.doi.org/10.21535%2FProICIUS.2012.v8.774
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