Design and Implementation of Multi-Antenna In-Band Full-Duplex Communication Device

Author(s):  
Jungbo Son ◽  
Donghyuk Gwak ◽  
Hyungsik Ju
IEEE Access ◽  
2020 ◽  
Vol 8 ◽  
pp. 163594-163607
Author(s):  
Sergey Shaboyan ◽  
Alireza S. Behbahani ◽  
Ahmed M. Eltawil

2011 ◽  
Vol 291-294 ◽  
pp. 2658-2661 ◽  
Author(s):  
Xiao Chun Tian ◽  
Jie Li ◽  
Yu Bao Fan ◽  
Xi Ning Yu ◽  
Jun Liu

SPI (Serial Peripheral Interface) is a full-duplex serial communication interface bus. Now, many devices adopt SPI. However, in many other aspects, microcontroller and microprocessor have no SPI interface, data transmission is inconvenient. With the development of FPGA technology, the problem can be solved absolutely by the I/O port of FPGA. In this paper, after introducing the principle of SPI, we designed SPI interface with FPGA and implemented the communication between SPI interface and the device of CRG20 which has a SPI interface. The algorithm of design SPI interface through FPGA is implemented with VHDL. The results of simulation in Quartus II and FPGA simulation are also described. The SPI bus interface modules fulfill the goal demanded.


IEEE Access ◽  
2017 ◽  
Vol 5 ◽  
pp. 14930-14942 ◽  
Author(s):  
Wooyeol Choi ◽  
Jaehyoung Park ◽  
Yonggang Kim ◽  
Ashutosh Sabharwal ◽  
Hyuk Lim

2016 ◽  
pp. 402-428
Author(s):  
Katsuyuki Haneda ◽  
Mikko Valkama ◽  
Taneli Riihonen ◽  
Emilio Antonio-Rodriguez ◽  
Dani Korpi

Author(s):  
Catur Wirawan Wijiutomo ◽  
Endro Ariyanto

Aircraft Data Network (ADN) is a data communication developed specifically for the aircraft environment. In such environments required data communication system that can work in real time and has a high level of reliability. One of the standards in ADN is Avionics Full-Duplex Switched Ethernet (AFDX) based on the ARINC 664 specification that is data communication standard for ADN that uses IEEE 802.3 standard on physical layer 1 and 2. It becomes the gap and challenge to implement the standard on the component of COTS By utilizing Linux-based embedded systems. The features designed and implemented in this paper are the switching and fault tolerant data components of ARINC 664. From the tests obtained, several results show that ADN functional features can be implemented and can simulate ADN mechanisms including fault tolerance capabilities. But there are performance limitations that the average jitter value of 3380 microseconds obtained has not met the requirements for use on aircraft that should be in the range of 500 microseconds.


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