Wavelength Conversion of High-Speed Phase and Intensity Modulated Signals Using a Highly Nonlinear Chalcogenide Glass Chip

2010 ◽  
Vol 22 (1) ◽  
pp. 3-5 ◽  
Author(s):  
M. D. Pelusi ◽  
F. Luan ◽  
S. Madden ◽  
D.-Y. Choi ◽  
D. A. Bulla ◽  
...  
2006 ◽  
Vol 14 (22) ◽  
pp. 10371 ◽  
Author(s):  
Vahid G. Ta'eed ◽  
Libin Fu ◽  
Mark Pelusi ◽  
Martin Rochette ◽  
Ian C. Littler ◽  
...  

Author(s):  
M. Galili ◽  
L.K. Oxenlowe ◽  
D. Zibar ◽  
A.T. Clausen ◽  
P. Jeppesen ◽  
...  

2014 ◽  
Vol 47 (2) ◽  
pp. 351-361 ◽  
Author(s):  
Nabil Sayed Abdel-Moneim ◽  
Christopher J. Mellor ◽  
Trevor M. Benson ◽  
David Furniss ◽  
Angela B. Seddon

2013 ◽  
Vol 52 (11) ◽  
pp. 116112 ◽  
Author(s):  
Md. Imran Hasan ◽  
Md. Samiul Habib ◽  
Md. Selim Habib ◽  
S. M. Abdur Razzak

2011 ◽  
Vol 28 (9) ◽  
pp. 2284 ◽  
Author(s):  
Tomas Kohoutek ◽  
Xin Yan ◽  
Teruo W. Shiosaka ◽  
Spyros N. Yannopoulos ◽  
Athanassios Chrissanthopoulos ◽  
...  

Author(s):  
Patrick J. O’Heron ◽  
Parviz E. Nikravesh ◽  
Ara Arabyan ◽  
Donald L. Kunz

Abstract A model is presented that can be used to simulate the highly nonlinear transient dynamics associated with advanced rotorcraft conversion processes. Multibody equations of motion of the fuselage, the tilting wing, and the rotor assembly are derived using a minimal set of coordinates. An enhanced aerodynamics model is employed to account for unsteadiness and nonlinearity in the near-wake aerodynamics, with a dynamic uniform inflow to compute the far-wake aerodynamics, and a flight control system is employed to compute the blade pitch settings that are necessary to achieve a desired flight path. The model is subjected to a demanding flight path simulation to illustrate that it can perform vertical take-off, hover, tilt-wing conversion, and high-speed forward flight maneuvers effectively.


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