Wireless Communications: Principles and Practice
Wireless Communications: Principles and Practice
Wireless Infrared Communications
Wireless Infrared Communications
Advanced Wireless Communications: 4G Technologies
Advanced Wireless Communications: 4G Technologies
Next Generation Mobile Access Technologies: Implementing TDD
Next Generation Mobile Access Technologies: Implementing TDD
Busy bursts for trading off throughput and fairness in cellular OFDMA-TDD
EURASIP Journal on Wireless Communications and Networking - Special issue on fairness in radio resource management for wireless networks
Contention free inter-cellular slot reservation
IEEE Communications Letters
Analysis of TDD Cellular Interference Mitigation Using Busy-Bursts
IEEE Transactions on Wireless Communications
Fundamental analysis for visible-light communication system using LED lights
IEEE Transactions on Consumer Electronics
A physical model of the wireless infrared communication channel
IEEE Journal on Selected Areas in Communications
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In this paper, first, path loss models are developed for infrared optical wireless transmission inside an aircraft cabin. Second, a cellular network in the aircraft is considered and signal-to-interference ratio (SIR) maps are determined via simulation. For this purpose, a Monte Carlo ray-tracing (MCRT) simulation is performed in a geometric computer-aided design (CAD) cabin model with defined position, azimuth (AZ), elevation (EL) and field of view (FOV) properties of transmitters and receivers. Mathematical models are developed for line-of-sight (LOS) and non-line-of-sight (NLOS) path losses along particular paths, including estimation of the path loss exponent and the shadowing component. The shadowing is modeled according to a log-normal distribution with zero mean and standard deviation σ. The validity of this model is confirmed in the paper. It is shown that irradiance distribution under LOS conditions experiences an attenuation with a path loss exponent of 1.92 and a shadowing standard deviation of 0.81dB. In NLOS conditions, however, the path loss exponent varies, depending on the nature of the NLOS cases considered. The presented NLOS scenarios yield path loss exponent values of 2.26 and 1.28, and shadowing standard deviation values of 1.27dB and 0.7dB, respectively. Finally, the cabin is divided into cells and SIR maps are presented for different frequency reuse factors. It is shown that at the edges of the circular cells with diameter of 2.8m, a SIR of -5.5dB is achieved in a horizontal cross section of the cabin for frequency reuse of 1, and -2dB and 3dB for frequency reuse factors of 2 and 3, respectively. This means that in an aircraft cabin, for reuse factors less than three, viable communication at the cell edges is not feasible without additional interference avoidance or interference mitigation techniques.