[1992 Proceedings] Vehicular Technology Society 42nd VTS Conference - Frontiers of Technology
DOI: 10.1109/vetec.1992.245268
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A simplified stochastic model for the aeronautical mobile radio channel

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Cited by 37 publications
(15 citation statements)
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“…In [95], the stochastic model was designed for characterizing the AG propagation in terms of transmission coefficients assuming that the quadrature components reflected from the ground surface can be modeled as a zero-mean Gaussian process. Also, Doppler spectrum analysis was performed for the diffuse multipath components.…”
Section: B Stochastic Channel Modelmentioning
confidence: 99%
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“…In [95], the stochastic model was designed for characterizing the AG propagation in terms of transmission coefficients assuming that the quadrature components reflected from the ground surface can be modeled as a zero-mean Gaussian process. Also, Doppler spectrum analysis was performed for the diffuse multipath components.…”
Section: B Stochastic Channel Modelmentioning
confidence: 99%
“…• Characterization of multipath components can be done with both numerical [95]- [96] and empirical analysis [13]- [15] Geometry-based stochastic • 3D channel characterization is possible with less environmental parameters to study the channel state information in UAV propagation for e.g. angular information due to spatial-temporal variations without considering non-stationarity in the UAV channel [16], [18] • Accuracy is dependent on the distribution of scatters confined in a target area of specific shapes…”
Section: Vmentioning
confidence: 99%
“…The dynamic nature of the aircraft motion and the rapidly changing environment generate varying channel characteristics that are categorized by different types of fading, Doppler Spread and system delays [132], [133], [134]. The take-off and landing speeds are in the range of 100-170 nautical miles/h while the other phases of flight will have a traveling speed of 600 nautical miles/h [135].…”
Section: A Challenges In Channel Modelingmentioning
confidence: 99%
“…ϕ aL is the lowest angle and ϕ aH is the highest angle of arrival signals from the aircraft antenna to the ground base station antenna. In [12], a beamwidth of Λ ≤ 360…”
Section: Dopplermentioning
confidence: 99%